Investigation at Transonic Speeds of Loading Over a 30o Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Mounted on a Body

Donald D. Arabian (Langley Aeronautical Laboratory, Langley Field, Va.)
naca-rm-l57g09a
1957


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-l57g09a.pdf