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Simulated Hypersonic Flows About A Blunt BodyUnsteady and steady flows compared. Report describes computer numerical study of two-dimensional, unsteady, viscous, hypersonic flows of air about blunt body with impinging shock. This kind of flow represents many practical phenomena; for example, interaction of fluctuating bow shock of hypersonic airplane with shocks of leading edge of wing or of lip of cowl at inlet to engine. Such interactions give rise to complicated, moving shock-on-shock patterns.
Document ID
19900000361
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kutler, P. (NASA Ames Research Center, Moffett Field, CA.)
Yee, H. C. (NASA Ames Research Center, Moffett Field, CA.)
Klopfer, G. H. (NEAR, Inc.)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 7
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
Report Number: ARC-12251
ISSN: 0145-319X
ARC-12251
Accession Number
90B10361
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitleN88-22650/TBSee AlsoNumerical Study Of Unsteady Viscous Hypersonic Blunt Body Flows With An Impinging Shock
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