A novel flux splitting scheme with robustness and low dissipation for hypersonic heating prediction-Reference-Cited by-同舟云学术

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A novel flux splitting scheme with robustness and low dissipation for hypersonic heating prediction

Published:2018-12 Issue: Volume:127 Page:126-137
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Chen Shu-sheng,Yan Chao,Zhong Kang,Xue Hai-chao,Li Er-long

Funder

National Natural Science Foundation of China

Academic Excellence Foundation of BUAA

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference47 articles.

1. Critical hypersonic aerothermodynamic phenomena;Bertin;Ann. Rev. Fluid Mech.,2006

2. K.A. Hoffmann, M.S. Siddiqui, S.T. Chiang, Difficulties associated with the heat flux computations of high speed flows by the Navier-Stokes equations, AIAA paper 91-0467, 1991.

3. Aerothermodynamics of blunt body entry vehicles;Hollis;Prog. Aerosp. Sci.,2012

4. G.H. Klopfer, H.C. Yee, Viscous hypersonic shock-on-shock interaction on blunt cowl lips, AIAA paper 88-0233, 1988.

5. J.H. Lee, O.H. Rho, Accuracy of AUSM+ scheme in hypersonic blunt body flow calculations, AIAA paper 98-1538, 1998.

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