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Volumn , Issue , 2002, Pages

Receptivity and linear stability of Stetson's mach 8 blunt cone stability experiments

Author keywords

[No Author keywords available]

Indexed keywords

AXISYMMETRIC FLOW; DISTURBANCE WAVES; ENVIRONMENTAL DISTURBANCES; FINITE DIFFERENCE SCHEME; LINEAR STABILITY; MODE EXCITATION; NUMERICAL RESULTS; NUMERICAL SIMULATION STUDIES;

EID: 84896693093     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (23)

References (28)
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  • 8
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    • Maslov, A.A.1    Shiplyuk, A.N.2    Sidorenko, A.3    Arnal, D.4
  • 13
    • 34250888431 scopus 로고
    • Entropy- and Boundary Layer Instability of Hypersonic Cone Flows - Fffirfts of Mean Flow Variations
    • Vol. Sendai/Japan, September 1994, Springer-Verlag, Berlin
    • Kufner, E. and Dallmaun, U., " Entropy- and Boundary Layer Instability of Hypersonic Cone Flows - Fffirfts of Mean Flow Variations," IU- TAM Symposium on Laminar- Turbulent Transition, Vol. Sendai/Japan, September 1994,pp. 197-204, Springer-Verlag, Berlin, 1994.
    • (1994) IU- TAM Symposium On Laminar- Turbulent Transition , pp. 197-204
    • Kufner, E.1    Dallmaun, U.2
  • 14
    • 0004194317 scopus 로고
    • Hypersonic Stability and TVansi- Tion
    • Eds. J.-A. Desideri, R. Glowinski, and J. Periaux, Springer-Verlag
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    • (1991) In Hypersonic Flows For Reentry Problems , vol.1 , pp. 18-34
    • Reshotko, E.1
  • 16
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    • Leading-Edge Receptivity to Free Stream Disturbance Waves for Hypersonic Flow Over A Parabola
    • Zhong, X., "Leading-Edge Receptivity to Free Stream Disturbance Waves for Hypersonic Flow Over A Parabola," Journal of Fluid Mechanics, Vol. 441,2001, pp. 315-367.
    • (2001) Journal of Fluid Mechanics , vol.441 , pp. 315-367
    • Zhong, X.1
  • 20
    • 84983126633 scopus 로고    scopus 로고
    • Direct Numerical Simulation cf Hypersonic Boundary-Layer Transition Over Blunt Leading Edges, Part I: New Numerical Methcds and Validation (Invited)
    • AZAA puper 97-0755, January 6-9, Reno, Nevada
    • Zhong, X., " Direct Numerical Simulation cf Hypersonic Boundary-Layer Transition Over Blunt Leading Edges, Part I: New Numerical Methcds and Validation (Invited)," AZAA puper 97-0755, 35th AZAA Aerospace Sciences Meeting and Exhibit, January 6-9, Reno, Nevada, 1997.
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  • 21
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    • August
    • Zhong, X.," High-Order Finite-Difference Schemes for Numerical Simulation of Hypersonic Boundary- Layer Transition," Journal f Computational Physics, Vol. 144, August 1998, pp. 662-709.
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  • 23
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  • 26
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.