Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 /

Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 /

Bibliographic Details
Main Author: Rivera, José A.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Format: Government Document Book
Language:English
Published: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1989.
Series:NASA technical memorandum ; 4094.
Subjects:
Flutter (Aerodynamics)
Aeroelasticity.
Airplanes > Wings, Rectangular.

Evans: US Documents Microfiche (3rd floor)

Holdings details from Evans: US Documents Microfiche (3rd floor)
Call Number: NAS 1.15:4094
 
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NAS 1.15:4094 Available