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Application of Lax's finite-difference method to nonequilibrium hypersonic flow problemsFinite difference method for unsteady flows applied to steady state equations for supersonic region of inviscid flow past two-dimensional and axisymmetric bodies
Document ID
19660011753
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
De Jarnette, F. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TR-R-234
Report Number: NASA-TR-R-234
Accession Number
66N21042
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FINITE DIFFERENCE METHOD
TWO-DIMENSIONAL BODY
INVISCID FLOW
STEADY STATE
AXISYMMETRIC BODY
UNSTEADY FLOW

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