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Sonic boom measurements from accelerating supersonic tracked sledsSupersonic sled tests on the Sandia 1524-m (5000-ft) track generate sonic booms of sufficient intensity to allow some airblast measurements at distance scales not obtained from wind tunnel or flight tests. During acceleration, an emitted curved boom wave propagates to a caustic, or focus. Detailed measurements around these caustics may help to clarify the overpressure magnification which can occur from real aircraft operations. Six fixed pressure gages have been operated to document the general noise field, and a mobile array of twelve gages.
Document ID
19740008612
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reed, J. W.
(Sandia National Labs. Albuquerque, NM, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Aircraft
Report/Patent Number
NASA-CR-132388
SLA-73-714
Report Number: NASA-CR-132388
Report Number: SLA-73-714
Accession Number
74N16725
Funding Number(s)
CONTRACT_GRANT: NASA ORDER L-75054
CONTRACT_GRANT: AT(29-1)-789
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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