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Nonlinear problems in wave propagationTheoretical predictions of weak shocks and Prandtl-Meyer expansions in unsteady flow and three-dimensional steady supersonic flow
Document ID
19670021577
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Oswatitsch, K. (VIENNA INST. OF TECH.)
Date Acquired
September 2, 2013
Publication Date
January 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-60079
SSS-67-74
Report Number: NASA-TM-X-60079
Report Number: SSS-67-74
Accession Number
67N30906
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK
THREE-DIMENSIONAL FLOW
PRANDTL-MEYER EXPANSION
UNSTEADY FLOW

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