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Development of atmospheric gust criteria for supersonic inlet designTechnique for relating transient tolerances in inlet throat Mach number and shock position to supersonic unstart frequency due to atmospheric turbulence for supersonic inlet design
Document ID
19710028359
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barry, F. W.
(Hamilton Standard Windsor Locks, CT, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1968
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-114372
HSER-5195
Report Number: NASA-CR-114372
Report Number: HSER-5195
Accession Number
71N37835
Funding Number(s)
CONTRACT_GRANT: NAS2-4515
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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