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F-8 refueling boom ground vibration testA ground vibration test was conducted on a simulated refueling boom mounted on an F-8 airplane. The ground vibration test was conducted to determine if the refueling boom modal frequencies were close to the airplane frequencies. The data presented in this report include modal frequencies, mode shape data, and structural damping coefficients.
Document ID
19850007404
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kahoe, M. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-84914
NAS 1.15:84914
H-1194
Report Number: NASA-TM-84914
Report Number: NAS 1.15:84914
Report Number: H-1194
Accession Number
85N15713
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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