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Structural dynamic stability augmentation and gust alleviation of flexible aircraft.Flexible aircraft response reduction to atmospheric turbulence, noting structural dynamic stability augmentation and gust alleviation
Document ID
19680064036
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wykes, J. H.
Date Acquired
August 4, 2013
Publication Date
October 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 68-1067
Report Number: AIAA PAPER 68-1067
Meeting Information
Meeting: ANNUAL MEETING AND TECHNICAL DISPLAY
Location: PHILADELPHIA, PA
Start Date: October 21, 1968
End Date: October 24, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A45008
Funding Number(s)
CONTRACT_GRANT: NAS4-1175
CONTRACT_GRANT: AF 33/615/-3133
CONTRACT_GRANT: AF 33/615/-1821
Distribution Limits
Public
Copyright
Other

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