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Computed Hypersonic Flow About A Sharp ConeReport describes mostly computational study of hypersonic flow about sharp cone. Part of continuing effort to understand and predict complicated aerodynamic and heat-transfer phenomena in flows over forebodies of such hypersonic vehicles as Space Shuttle and proposed National Aerospace Plane. Focuses on transition from laminar to turbulent flow, with particular reference to heat-transfer predictions.
Document ID
19910000538
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Kaul, Upender K.
(Sterling Software)
Date Acquired
August 14, 2013
Publication Date
October 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 10
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12675
Report Number: ARC-12675
ISSN: 0145-319X
Accession Number
91B10538
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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