Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7
By: Jose A. Rivera, Jr.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4094.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Flutter (Aerodynamics); Aeroelasticity.; Airplanes -- Wings, Rectangular.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1989. 1 microfiche.