Simulation of hypersonic shock wave/boundary layer interaction using high order WENO scheme

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Citations (Scopus)

Abstract

This paper investigates the accuracy and robustness of high order WENO schemes for predicting hypersonic shock wave/boundary layer interaction. The implicit time marching method with unfactored Gauss-Seidel line relaxation is used with a 5th order WENO finite difference scheme for inviscid fluxes. The viscous terms are discretized using a 4th order conservative central differencing. Numerical results agree well with the experiment of a hollow/flare geometry at Mach number of 12.49 and Reynolds number of 1.09 × 10 5/ft.

Original languageEnglish
Title of host publication48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
StatePublished - Dec 13 2010
Event48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, FL, United States
Duration: Jan 4 2010Jan 7 2010

Other

Other48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
CountryUnited States
CityOrlando, FL
Period1/4/101/7/10

Fingerprint

Hypersonic aerodynamics
Shock waves
Mach number
Boundary layers
Reynolds number
Fluxes
Geometry
Experiments

ASJC Scopus subject areas

  • Aerospace Engineering

Cite this

Shen, Y., Zha, G., & Huerta, M. (2010). Simulation of hypersonic shock wave/boundary layer interaction using high order WENO scheme. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition [2010-1047]

Simulation of hypersonic shock wave/boundary layer interaction using high order WENO scheme. / Shen, Yiqing; Zha, GeCheng; Huerta, Manuel.

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. 2010-1047.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shen, Y, Zha, G & Huerta, M 2010, Simulation of hypersonic shock wave/boundary layer interaction using high order WENO scheme. in 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition., 2010-1047, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, FL, United States, 1/4/10.
Shen Y, Zha G, Huerta M. Simulation of hypersonic shock wave/boundary layer interaction using high order WENO scheme. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. 2010-1047
Shen, Yiqing ; Zha, GeCheng ; Huerta, Manuel. / Simulation of hypersonic shock wave/boundary layer interaction using high order WENO scheme. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010.
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