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Volumn 34, Issue 4, 1996, Pages 764-771

Simulation of multiple shock-shock interference patterns on a cylindrical leading edge

Author keywords

[No Author keywords available]

Indexed keywords


EID: 3242835265     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13138     Document Type: Article
Times cited : (16)

References (28)
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    • Wieting, A.R.1    Holden, M.S.2
  • 13
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    • also AIAA Paper 91-1800, June 1991
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  • 14
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    • Oct.
    • Roe, P. L., "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Vol. 43, Oct. 1981, pp. 357-372.
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    • March
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    • Jan.
    • Van Albada, G. D., Van Leer, B., and Roberts, W. W., "A Comparative Study of Computational Methods in Cosmic Gas Dynamics," Astronomy and Astrophysics, Vol. 108, Jan. 1982, pp. 76-84.
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  • 22
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    • A Numerical Technique for Two-Dimensional Grid Generation with Grid Control at All of the Boundaries
    • Oct.
    • Hsu, K., and Lee, S., "A Numerical Technique for Two-Dimensional Grid Generation with Grid Control at All of the Boundaries," Journal of Computational Physics, Vol. 96, Oct. 1991, pp. 451-469.
    • (1991) Journal of Computational Physics , vol.96 , pp. 451-469
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  • 23
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    • private communication, Univ. of Texas at Arlington, TX, Dec.
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  • 24
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    • Application of Essentially Nonoscillatory Scheme to Unsteady Hypersonic Shock-Shock Interference Heating Problems
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  • 26
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    • Numerical Study of Transient Flow Phenomena in Shock Tunnels
    • Tokarcik-Polsky, S., and Cambier, J. L., "Numerical Study of Transient Flow Phenomena in Shock Tunnels," AIAA Journal, Vol. 32, No. 5, 1994, pp. 971-978.
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    • Tokarcik-Polsky, S.1    Cambier, J.L.2
  • 27
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    • The Starting Process in a Hypersonic Nozzle
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.