Bending-Torsion Flutter Calculations Modified by Subsonic Compressibility Corrections
Description:
From Summary: "A number of calculations of bending-torsion wing flutter are made at two Mach numbers, m=0 (incompressible case) and m=0.7, and results are compared. The air forces employed for the case of m=0.7 are based on Frazer's recalculation of Possio's results, which are derived on the assumption of small disturbances to the main flow. For ordinary wings of normal density and of low bending frequency in comparison with torsion frequency, the compressibility correction to the flutter speed…
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Date:
December 18, 1945
Creator:
Garrick, I. E.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department