3 edition of Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 found in the catalog.
Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7
Rivera, JoseМЃ A.
by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service] in [Washington, DC], [Springfield, Va
Written in English
|Statement||Jose A. Rivera, Jr.|
|Series||NASA technical memorandum -- 4094.|
|Contributions||United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.|
|The Physical Object|
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