Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. - Contributor
Publication
1989 - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL17660209M
Subjects
Topics
AirplanesAeroelasticityRectangular wingsWings, RectangularFlutter (Aerodynamics)Airplanes -- Wings, Rectangular
Series Statement
- NASA technical memorandum -- 4094.
Other Editions
- Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7
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