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Multidomain approach for calculating compressible flowsA multidomain approach for calculating compressible flows by using unsteady or pseudo-unsteady methods is presented. This approach is based on a general technique of connecting together two domains in which hyperbolic systems (that may differ) are solved with the aid of compatibility relations associated with these systems. Some examples of this approach's application to calculating transonic flows in ideal fluids are shown, particularly the adjustment of shock waves. The approach is then applied to treating a shock/boundary layer interaction problem in a transonic channel.
Document ID
19820022410
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cambier, L.
(NASA Headquarters Washington, DC United States)
Chazzi, W.
(NASA Headquarters Washington, DC United States)
Veuillot, J. P.
(NASA Headquarters Washington, DC United States)
Viviand, H.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-76692
NAS 1.15:76692
Report Number: NASA-TM-76692
Report Number: NAS 1.15:76692
Accession Number
82N30286
Funding Number(s)
CONTRACT_GRANT: NASW-3541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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