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A wind-tunnel technique for measuring frequency-response functions for gust load analyses.Wind tunnel technique for measuring frequency response of flexible airplane to vertical sinusoidal gusts
Document ID
19670034179
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bennett, R. M.
Gilman, J., Jr.
Date Acquired
August 3, 2013
Publication Date
December 1, 1966
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 65-787
Report Number: AIAA PAPER 65-787
Accession Number
67A12908
Distribution Limits
Public
Copyright
Other
Keywords
FREQUENCY RESPONSE
WIND TUNNEL STABILITY TEST
VERTICAL AIR CURRENT
GUST LOAD

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