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A method for predicting full scale buffet response with rigid wind tunnel model fluctuating pressure data. Volume 2: Power spectral densities for method assessmentThe predicted upper and lower bounds power spectra for all of the cases and response items given in Volume 1 are plotted. The flight test power spectra are shown on each prediction plot for the nominal value of angle of attack that most closely agrees with the flexible angle for the prediction. The flight test and prediction conditions are given in tabular form for all cases considered.
Document ID
19790005850
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cunningham, A. M., Jr.
(General Dynamics/Fort Worth TX, United States)
Benepe, D. B.
(General Dynamics/Fort Worth TX, United States)
Watts, D.
(General Dynamics/Fort Worth TX, United States)
Waner, P. G.
(General Dynamics/Fort Worth TX, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3036
Report Number: NASA-CR-3036
Accession Number
79N14021
Funding Number(s)
CONTRACT_GRANT: NAS2-7091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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