Tomeki

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

By Rivera, José A.

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Publish Date

1989

Publisher

National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,For sale by the National Technical Information Service]

Language

eng

Pages

-