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Inviscid transonic flow computations with shock fittingFirst- and second-order numerical procedures for calculating two-dimensional transonic flows that treat shock waves as discontinuities are discussed. This short communication illustrates their application to a simple but non-trivial problem for which there are limited theoretical results.
Document ID
19760044907
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Yu, N. J. (Arizona Univ. Tucson, AZ, United States)
Seebass, A. R. (Arizona, University Tucson, Ariz., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Meeting Information
Meeting: Symposium Transsonicum II
Location: Goettingen
Start Date: September 8, 1975
End Date: September 13, 1975
Accession Number
76A27873
Funding Number(s)
CONTRACT_GRANT: NGR-33-010-057
Distribution Limits
Public
Copyright
Other

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