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Lateral-spread sonic-boom ground-pressure measurements from airplanes at altitudes to 75,000 feet and at mach numbers to 2.0Measurements of shock wave overpressures from airplanes at altitudes to 75,000 feet & supersonic speed
Document ID
19640000542
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Copeland, W. L. (NASA Langley Research Center Hampton, VA, United States)
Hilton, D. A. (NASA Langley Research Center Hampton, VA, United States)
Maglieri, D. J. (NASA Langley Research Center Hampton, VA, United States)
Parrott, T. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1963
Subject Category
Biosciences
Report/Patent Number
NASA-TN-D-2021
Report Number: NASA-TN-D-2021
Accession Number
64N10451
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HIGH ALTITUDE PRESSURE
SONIC BOOM
SUPERSONIC AIRCRAFT

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