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Investigation of sonic boom generated by thin, nonlifting, rectangular wingsA theory is described for predicting sonic boom pressure signatures emitted by nonlifting rectangular wings. Comparisons are made with previous (Whitham) theory and with experimentally determined near field signatures. Although both theories agree with experiment for low aspect ratio wings, Whitman's theory seriously overpredicts signature length for high aspect ratio wings. No experiments were conducted in the far field, but the two theories predict nearly identical results in this region.
Document ID
19720004300
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Davis, S. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-6619
A-4109
Report Number: NASA-TN-D-6619
Report Number: A-4109
Accession Number
72N11949
Funding Number(s)
PROJECT: RTOP 136-13-02-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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