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Evaluation of certain minimum boom conceptsSonic boom efficiency factor analyses for rectangular configuration, high aspect ratio arrow wing, and delta wing models
Document ID
19680025440
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Henderson, H. R. (NASA Langley Research Center Hampton, VA, United States)
Runyan, H. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Publication Information
Publication: 2ND CONF. ON SONIC BOOM RES. 1968
Subject Category
Aircraft
Accession Number
68N34912
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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