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Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:28:55Z
date available2017-09-04T18:28:55Z
date copyright01/01/1980
date issued1980
identifier otherIRYKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/211072
description abstractA numerically generated orthogonal coordinate system (with the body surface and shock wave as opposite boundaries) was applied with a time asymptotic method to obtain steady flow solutions for axisymmetric inviscid flow over several blunt bodies including spheres, paraboloids, ellipsoids, hyperboloids, hemisphere cylinders, spherically blunted cones, and a body with a concavity in the stagnation region. Comparisons with experimental data and with the results of other computational methods are discussed. The numerically generated orthogonal coordinate system is described and applications of the method to complex body shapes, particularly those with concave regions, are discussed.
languageEnglish
titleNASA-TP-1619num
titleApplication of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodiesen
typestandard
page62
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1980
contenttypefulltext
subject keywordsBLUNT
subject keywordsBODIES
subject keywordsBOUNDARY
subject keywordsCOORDINATES
subject keywordsDISTRIBUTION
subject keywordsFLOW
subject keywordsGENERATION
subject keywordsGRID
subject keywordsINVISCID
subject keywordsMATHEMATICS
subject keywordsORTHOGONALITY
subject keywordsPROBLEMS
subject keywordsSHOCK
subject keywordsSTEADY
subject keywordsSUPERSONIC
subject keywordsVALUE
subject keywordsWAVES


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