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An investigation of wing buffeting response at subsonic and transonic speeds. Phase 2: F-111A flight data analysis. Volume 2: Plotted power spectraPlotted power spectra for all of the flight points examined during the Phase 2 flight data analysis are presented. Detailed descriptions of the aircraft, the flight instrumentation and the analysis techniques are given. Measured and calculated vibration mode frequencies are also presented to assist in further interpretation of the PSD data.
Document ID
19780025174
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)
Traylor, S., 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-152113
Report Number: NASA-CR-152113
Accession Number
78N33117
Funding Number(s)
CONTRACT_GRANT: NAS2-7091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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