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IN-FLIGHT SHOCK-WAVE PRESSURE MEASUREMENTS ABOVE AND BELOW A BOMBER AIRPLANE AT MACH NUMBERS FROM 1.42 TO 1.69In-flight shock wave pressure measurements above and below bomber aircraft at mach 1.42 to 1.69
Document ID
19630013245
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bryant, J. F., Jr. (NASA Langley Research Center Hampton, VA, United States)
Maglieri, D. J. (NASA Langley Research Center Hampton, VA, United States)
Ritchie, V. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1963
Subject Category
Biosciences
Report/Patent Number
NASA-TN-D-1968
Report Number: NASA-TN-D-1968
Accession Number
63N23125
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOMBER AIRCRAFT
PRESSURE MEASUREMENT
FLIGHT TEST
SHOCK WAVE

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