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A CALCULATION METHOD FOR SOLVING AEROELASTIC PROBLEMS FOR STUB WINGS AND ENTIRE AIRCRAFTCalculation method for solving aeroelastic problems for stub wings and entire aircraft
Document ID
19630012385
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kussner, H. G.
Date Acquired
August 1, 2013
Publication Date
September 1, 1963
Subject Category
Auxiliary Systems
Accession Number
63N22265
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRCRAFT DESIGN
WING
AEROELASTICITY
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