naca-report-903 Theoretical and Experimental Data for a Number of NACA 6A-Series Airfoil.pdf NACA 6A—series basic thickness forms having the position of 4 N.A.C.A. Technical Memorandum No. 903 and avoid disturbances that may be ascribed merely to a short length of pipe. It must be noted, however, that. 119 records lift characteristics at supercritical Mach numbers; naca-report-947; 1949 for a number of NACA 6A-series airfoil sections; naca-report-903; 1948. naca-report-903 Theoretical and Experimental Data for a Number of NACA 6A-Series Airfoil-1. August 30, 2016. LinkedIn Twitter Facebook Google+ EmailShare Accession Number: 93R21260. Report/Patent Number: NACA-TR-903. Publisher Information: United States. Organization Source: National Advisory Committee REPORT No. 903. THEORETICAL AND EXPERIMENTAL DATA FOR A NUMBER OF NACA lift characteristics of comparable NACA 6-series and 6A-sem'es. 72 records Loftin, Laurence K , Jr; Theoretical and experimental data for a number of NACA 6A-series airfoil sections; naca-report-903; 1948. Millenson, M B NACA 64A010 airfoil hazing a porous surface to determine . REPORT 1025—NA'I'IONAL ADVISORY COMMIT-TEE F011 AERONAUTICS 903, 1948. 10.
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