A preliminary study of relaxation methods for the inviscid conservative gasdynamics equations using flux splitting / Joseph L. Steger ; prepared for Langley Research Center under contract NAS1-15852.

Plus minus flux vector split schemes are combined with the multigrid relaxation method to obtain fast rates of iterative (or steady state) convergence. On model nonlifting biconvex airfoil flow, steady state convergence is obtained using multigrid in 40 iteractions for subsonic cases and in 120 ite...

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Main Author: Steger, Joseph L.
Corporate Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center, Flow Simulations, Inc
Format: Government Document Book
Language:English
Published: Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981.
Series:NASA contractor report ; NASA CR-3415.
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Call Number: NAS 1.26:3415
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Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number: NAS 1.26:3415
NAS 1.26:3415 Available Place a Hold