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

An edition of Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7 (1989)

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

By Jose A. Rivera

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Publish Date

1989

Publisher

Langley Research Center

Language

Pages

Description:

subjects: Flutter analysis, Spanwise curvature