Effects Of Structural Flexibility On Gust Loading Of Aircraft Part II: Dynamic Stresses In Swept-wing Airplanes

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Report Number: WADC TR 54-592 Part 2
Author(s): Kirsch, A. A., Foss, K. A., Calligeros, J. M.
Corporate Author(s): Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-08
Pages: 201
Contract: AF 33(616)-2425
DoD Project: None Given
PB Number: PB134845
Identifier: AD0078081

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Provenance: Lockheed Martin Missiles & Fire Control

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