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Inviscid transonic flow computations with shock fittingFirst-and second-order numerical procedures are presented for calculating two-dimensional transonic flows that treat shock waves as discontinuities. Their application to a simple but nontrivial problem for which there are limited theoretical results is discussed.
Document ID
19760003326
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yu, N. J. (Arizona Univ. Tucson, AZ, United States)
Seebass, A. R. (Arizona Univ. Tucson, AZ, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-145430
Report Number: NASA-CR-145430
Accession Number
76N10414
Funding Number(s)
CONTRACT_GRANT: NGR-33-010-057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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