DocumentCode :
2492799
Title :
Three-dimensional simulation of underexpanded plumes using upwind algorithms
Author :
Obayashi, Shigeru ; Gavali, Sharad
Author_Institution :
NASA Ames Res. Center, Moffett Field, CA, USA
fYear :
1988
fDate :
14-18 Nov 1988
Firstpage :
25
Abstract :
Different numerical techniques have been examined for simulating the underexpanded plumes in supersonic flows. The results revealed that the monotone differentiable limiter is superior to the TVD (total variation diminishing) minmod limiter when the MUSCL (monotonic upstream schemes for conservation laws) approach is used for Roe´s upwind scheme. Roe´s upwind scheme is found to be superior to the central difference scheme not only for capturing shock waves, but also for capturing shear flows
Keywords :
flow simulation; physics computing; supersonic flow; TVD; monotone differentiable limiter; shear flows; shock waves; supersonic flows; three dimensional simulation; total variation diminishing; underexpanded plumes; upwind algorithms; Aerodynamics; Aerospace simulation; Computational fluid dynamics; Computational modeling; NASA; Navier-Stokes equations; Propulsion; Shock waves; Space shuttles; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Supercomputing 88. Vol.II: Science and Applications., Proceedings
Conference_Location :
Orlando, FL
Print_ISBN :
0-8186-8923-4
Type :
conf
DOI :
10.1109/SUPERC.1988.74129
Filename :
74129
Link To Document :
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