Three-dimensional calculations of hypersonic flowfield over double-cone geometries
Author:
Affiliation:
1. Tohoku Univ., Sendai, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-647
Reference21 articles.
1. 2Nonaka, S., and Takayama, K. "Ballistic Range Measurement of Shock Shapes in Nonequilibrium Regime,"AIAAPaper 99-1025, 1999.
2. 3Niizuma, K., and Sawada, K. "Nonequilibrium Flow Computations forThe Space ShuttleNose Using Unstructured Meshes,"AIAAPaper 97-2548, 1997.
3. 4Wada, Y. and Liu, M. S. "A Flux Splitting Scheme with High-Resolution and Robustness for Discontinuities,"AIAAPaper 94-0083,1994.
4. 5Barth, T. J. "Aspect of Unstructured Grid and Finite-Volume Solvers forthe Euler and Navier-Stokes Equations,"AGARD-R-787, 1992, pp. 6/1-61.
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