Comparison of analytical and experimental steady- and unsteady-pressure distributions at Mach number 0.78 for a high-aspect-ratio supercritical wing model with oscillating control surfaces
By: William E. McCain
Contributors: Langley Research Center
Series: NASA technical memorandum -- 84589
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1983
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Oscillating wings (Aerodynamics); Airplanes -- Wings
Notes: "January 1983."

Bibliography: p. 17-18

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1985. 1 microfiche ; 11 x 15 cm