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March 3, 2015 20:00
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Error log when trying to use Xfoil_interaction.
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| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> | |
| =================================================== | |
| XFOIL Version 6.99 | |
| Copyright (C) 2000 Mark Drela, Harold Youngren | |
| This software comes with ABSOLUTELY NO WARRANTY, | |
| subject to the GNU General Public License. | |
| Caveat computor | |
| =================================================== | |
| File xfoil.def not found | |
| QUIT Exit program | |
| .OPER Direct operating point(s) | |
| .MDES Complex mapping design routine | |
| .QDES Surface speed design routine | |
| .GDES Geometry design routine | |
| SAVE f Write airfoil to labeled coordinate file | |
| PSAV f Write airfoil to plain coordinate file | |
| ISAV f Write airfoil to ISES coordinate file | |
| MSAV f Write airfoil to MSES coordinate file | |
| REVE Reverse written-airfoil node ordering | |
| DELI i Change written-airfoil file delimiters | |
| LOAD f Read buffer airfoil from coordinate file | |
| NACA i Set NACA 4,5-digit airfoil and buffer airfoil | |
| INTE Set buffer airfoil by interpolating two airfoils | |
| NORM Buffer airfoil normalization toggle | |
| HALF Halve the number of points in buffer airfoil | |
| XYCM rr Change CM reference location, currently 0.25000 0.00000 | |
| BEND Display structural properties of current airfoil | |
| PCOP Set current-airfoil panel nodes directly from buffer airfoil points | |
| PANE Set current-airfoil panel nodes ( 160 ) based on curvature | |
| .PPAR Show/change paneling | |
| .PLOP Plotting options | |
| WDEF f Write current-settings file | |
| RDEF f Reread current-settings file | |
| NAME s Specify new airfoil name | |
| NINC Increment name version number | |
| Z Zoom | (available in all menus) | |
| U Unzoom | | |
| XFOIL c> | |
| Enter filename s> | |
| File READ error. Unrecognizable file format | |
| *** LOAD NOT COMPLETED *** | |
| XFOIL c> | |
| *** No airfoil available *** | |
| XFOIL c> MACH command not recognized. Type a "?" for list | |
| XFOIL c> RE command not recognized. Type a "?" for list | |
| XFOIL c> VISC command not recognized. Type a "?" for list | |
| XFOIL c> PACC command not recognized. Type a "?" for list | |
| XFOIL c> AERO command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> ASEQ command not recognized. Type a "?" for list | |
| XFOIL c> 0 command not recognized. Type a "?" for list | |
| XFOIL c> 20 command not recognized. Type a "?" for list | |
| XFOIL c> 1 command not recognized. Type a "?" for list | |
| XFOIL c> | |
| XFOIL c> Traceback (most recent call last): | |
| File "main.py", line 79, in <module> | |
| genome = genetics.genetic_step(generation,num_parent, weighting_parameters) | |
| File "/home/juanlu/Development/Python/AeroPython/aeropy/aeropy/Xfoil_Interaction/Genetic_algorithm_files/genetics.py", line 36, in genetic_step | |
| scores = analyze.score(generation,num_pop, weights) | |
| File "/home/juanlu/Development/Python/AeroPython/aeropy/aeropy/Xfoil_Interaction/Genetic_algorithm_files/analyze.py", line 71, in score | |
| pop_results = pop_analice (generation, num_pop) | |
| File "/home/juanlu/Development/Python/AeroPython/aeropy/aeropy/Xfoil_Interaction/Genetic_algorithm_files/analyze.py", line 32, in pop_analice | |
| pop_results[profile_number - 1, :] = profile_analice (generation, profile_number) | |
| File "/home/juanlu/Development/Python/AeroPython/aeropy/aeropy/Xfoil_Interaction/Genetic_algorithm_files/analyze.py", line 45, in profile_analice | |
| datos = np.loadtxt(data_root, skiprows=12, usecols=[1,2]) | |
| File "/home/juanlu/.miniconda3/envs/py34/lib/python3.4/site-packages/numpy/lib/npyio.py", line 739, in loadtxt | |
| fh = iter(open(fname)) | |
| FileNotFoundError: [Errno 2] No such file or directory: 'aerodata/datagen0prof1.txt' |
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