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Tangent-ogive nose conesProgram calculates aerodynamic heating and shear stresses at wall for tangent-ogive noses that are slender enough to maintain an attached nose shock during portion of flight when heat transfer from boundary layer to wall is significant.
Document ID
19760000107
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Wing, L. D.
Date Acquired
August 8, 2013
Publication Date
March 1, 1976
Publication Information
Publication: NASA Tech Briefs
Volume: 1
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
GSC-11468
Accession Number
76B10107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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