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Ground measurements of shock-wave pressure for fighter airplanes flying at very low altitudes and comments on associated response phenomenaGround measurements of shock wave pressure for fighter aircraft at very low altitudes
Document ID
19650003204
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Huckel, V. (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
December 1, 1961
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-611
Report Number: NASA-TM-X-611
Accession Number
65N12805
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FIGHTER AIRCRAFT
SHOCK WAVE
LOW ALTITUDE
PRESSURE MEASUREMENT

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