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New implicit boundary procedures - Theory and applicationsAnalytical techniques for the application of implicit boundary conditions for inviscid flows to shock and body boundary layer conditions involving the Euler equations are presented. The theory of characteristics is used to update boundary points with spatial second order accuracy. The method is useful for implicit schemes which feature approximate factorization, and as such is incorporated into an existing PNS code. Examples are provided in terms of flows over a cone, over a maneuverable reentry vehicle, and over a finned vehicle. Improvements in the convergence rate are demonstrated for the conical flow solutions.
Document ID
19830035318
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rai, M. M.
(NASA Ames Research Center Moffett Field; Informatics General Corp., Palo Alto, CA, United States)
Chaussee, D. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 83-0123
Report Number: AIAA PAPER 83-0123
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A16536
Distribution Limits
Public
Copyright
Other

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