Simulation of axisymmetric scramjet inlet flow fields using anti-diffusive WENO Navier-Stokes solver-Reference-Cited by-同舟云学术

Simulation of axisymmetric scramjet inlet flow fields using anti-diffusive WENO Navier-Stokes solver

Published:2015-05 Issue:5 Volume:29 Page:1875-1882
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Huang Juan-Chen,Yang Jaw-Yen,Lai Yu-Hsuan,Guo Jeng-Shan

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.1007/s12206-015-0408-3.pdf

Reference22 articles.

1. D. Andreadis, Scramjets integrate air and space, The Industrial Physicist (2004).

2. F. Bouchut, An antidiffusive entropy scheme for monotone scalar conservation law, J. of Scientific Computing, 21 (2004) 1–30.

3. E. T. Curren and S. B. N. Murthy, Ed. scramjet propulsion, AIAA Progress in Astronautics and Aeronautics, 189 (2001) 447–512.

4. J. R. Henry, E. H. Jr. Andrews, S. Z. Pinckney and C. R. McClinton, Boundary layer and starting problems on a short axisymmetric scramjet inlet, Compressible Turbulent Boundary Layers, NASA SP-216 (1969) 481–508.

5. J. C. Huang, H. Lin and J. Y. Yang, Implicit preconditioned WENO schemes for steady viscous flows, J. Comput. Phys., 228 (2009) 420–438.

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