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Sonic boom reflection factors for flight near the threshold Mach numberIncident sonic boom shock wave reflection factors off smooth surface, discussing pressure rise and flight near threshold Mach number
Document ID
19710049913
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Thomas, C. L.
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Subject Category
Aircraft
Accession Number
71A30610
Distribution Limits
Public
Copyright
Other

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