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Influence of airplane configuration on sonic- boom characteristicsWind tunnel and flight testing of airplane configuration influence on sonic boom characteristics
Document ID
19640015089
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Carlson, H. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 2, 2013
Publication Date
January 29, 1964
Subject Category
Biosciences
Report/Patent Number
NASA-RP-208
Report Number: NASA-RP-208
Accession Number
64N25003
Distribution Limits
Public
Copyright
Other
Keywords
FLIGHT TEST
SONIC BOOM
WIND TUNNEL

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