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An investigation of wing buffeting response at subsonic and transonic speeds. Phase 1: F-111A flight data analysis. Volume 3: Tabulated power spectraVolume 3 of this three volume report is presented. This volume presents power spectral density in tabular form for the convenience of those who might wish to perform additional analysis. Some of the information contained in Volume 1 is again repeated (as in volume 2) in this volume to allow the reader to identify the specific conditions appropriate to each tabular listing and for further analysis.
Document ID
19780025172
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Benepe, D. B. (General Dynamics/Fort Worth TX, United States)
Cunningham, A. M., Jr. (General Dynamics/Fort Worth TX, United States)
Dunmyer, W. D. (General Dynamics/Fort Worth TX, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-152111
Report Number: NASA-CR-152111
Accession Number
78N33115
Funding Number(s)
CONTRACT_GRANT: NAS2-7091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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