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Volumn , Issue , 1998, Pages

Hypersonic boundary layer transition for X-33 phase II vehicle

Author keywords

[No Author keywords available]

Indexed keywords

HYPERSONIC FLOW; HYPERSONIC VEHICLES;

EID: 85088767552     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-867     Document Type: Conference Paper
Times cited : (34)

References (18)
  • 2
    • 0020183065 scopus 로고
    • Shuttle Boundary-Layer Transition Due to Distributed Roughness and Surface Cooling
    • Sep-Oct
    • Berlin, J. J., Hayden, T. E., and Goodrich, W. D., "Shuttle Boundary-Layer Transition Due to Distributed Roughness and Surface Cooling," Journal of Spacecraft and Rockets, Vol. 7, No. 3, Sep-Oct 1983, pp. 389-396.
    • (1983) Journal of Spacecraft and Rockets , vol.7 , Issue.3 , pp. 389-396
    • Berlin, J.J.1    Hayden, T.E.2    Goodrich, W.D.3
  • 12
    • 0028671360 scopus 로고
    • Data Parallel Lower-Upper Relaxation Method for Reacting Flows
    • December
    • Candler, G. V., Wright, M. J., and McDonald, J. D., "Data Parallel Lower-Upper Relaxation Method for Reacting Flows," AIAA Journal, Vol. 32, No. 12, December 1994, pp. 2380-2386.
    • (1994) AIAA Journal , vol.32 , Issue.12 , pp. 2380-2386
    • Candler, G.V.1    Wright, M.J.2    McDonald, J.D.3
  • 13
    • 0028423185 scopus 로고
    • Approximate Method for Calculating Heating Rates on Three-Dimensional Vehicles
    • May-June
    • Hamilton II, H. H., Greene, F. A., and DeJamette, F. R., "Approximate Method for Calculating Heating Rates on Three-Dimensional Vehicles," Journal of Spacecraft and Rockets, Vol. 31, No. 3, May-June 1994, pp. 345-354.
    • (1994) Journal of Spacecraft and Rockets , vol.31 , Issue.3 , pp. 345-354
    • Hamilton, H.H.1    Greene, F.A.2    DeJamette, F.R.3
  • 14
    • 0002887728 scopus 로고
    • Theory of Stagnation Point Heat Transfer in Dissociated Air
    • No. 2
    • Fay, J. A. and Ridell, F. R., "Theory of Stagnation Point Heat Transfer in Dissociated Air," Journal of Aeronautical Sciences, Vol. 15, No. 2, 1958.
    • (1958) Journal of Aeronautical Sciences , vol.15
    • Fay, J.A.1    Ridell, F.R.2
  • 16
    • 0029514350 scopus 로고
    • Three-Dimensional Boundary-Layer Transition on a Swept Wing at Mach 3. 5
    • November
    • Cattafesta III, L. N., Iyer, V., Masad, J. A., King, R. A., and Dagenhart, J. R., "Three-Dimensional Boundary-Layer Transition on a Swept Wing at Mach 3. 5," AIAA Journal, Vol. 33, No. 11, November 1995, pp. 2032-2037.
    • (1995) AIAA Journal , vol.33 , Issue.11 , pp. 2032-2037
    • Cattafesta, L.N.1    Iyer, V.2    Masad, J.A.3    King, R.A.4    Dagenhart, J.R.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.