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Effects Of Structural Flexibility On Gust Loading Of Aircraft Part I: Gust Loads On Swept-wing Airplanes Free To Pitch And To Deform Statically

Report Number: WADC TR 54-592 Part 1
Author: Foss, K. A.
Corporate Author: Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Pages: 116
Contract: AF 33(616)-2425
Project: None Given
PB Number: PB134995
AD Number: AD0084480

Abstract:
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Provenance:
Lockheed Martin Missiles & Fire Control
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