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Volumn , Issue , 2008, Pages

Implementation of a blowing boundary condition in the LAURA code

Author keywords

[No Author keywords available]

Indexed keywords

ABLATION; BOUNDARY CONDITIONS; MASS TRANSFER; NAVIER STOKES EQUATIONS;

EID: 77958476644     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-1243     Document Type: Conference Paper
Times cited : (49)

References (18)
  • 1
    • 0032676097 scopus 로고    scopus 로고
    • Aerothermodynamics of the stardust sample return capsule
    • Olynick, D., Chen, Y. K., and Taubet, M. E., "Aerothermodynamics of the Stardust Sample Return Capsule, ", Journal of Spacecraft and Rockets, Vol. 36, No. 3, pp. 442-462, 1999.
    • (1999) Journal of Spacecraft and Rockets , vol.36 , Issue.3 , pp. 442-462
    • Olynick, D.1    Chen, Y.K.2    Taubet, M.E.3
  • 2
    • 0035609342 scopus 로고    scopus 로고
    • Predictions of ablating hypersonic vehicles using an iterative coupled fluid/thermal approach
    • Kuntz, D.W., Hassan, B., and Potter, D.L., "Predictions of Ablating Hypersonic Vehicles Using an Iterative Coupled Fluid/Thermal Approach", Journal of Thermophysics and Heat Transfer, Vol. 15, No. 2, pp 129-139.
    • Journal of Thermophysics and Heat Transfer , vol.15 , Issue.2 , pp. 129-139
    • Kuntz, D.W.1    Hassan, B.2    Potter, D.L.3
  • 8
    • 0003808258 scopus 로고
    • Convective heat transfer with mass addition and chemical reactions
    • Pergamon Press, New York
    • Lees, L., "Convective Heat Transfer with Mass Addition and Chemical Reactions," Combustion and Propulsion, Third AGARD Colloquium, pp. 451-498, Pergamon Press, New York, 1959.
    • (1959) Combustion and Propulsion, Third AGARD Colloquium , pp. 451-498
    • Lees, L.1
  • 12
    • 0032637766 scopus 로고    scopus 로고
    • Ablation and thermal response program for spacecraft heatshield analysis
    • Chen, Y. K. and Milos, F. S., "Ablation and Thermal Response Program for Spacecraft Heatshield Analysis," Journal of Spacecraft and Rockets, Vol. 36, No. 3, pp. 475-483, 1999.
    • (1999) Journal of Spacecraft and Rockets , vol.36 , Issue.3 , pp. 475-483
    • Chen, Y.K.1    Milos, F.S.2
  • 15
    • 85007703995 scopus 로고
    • Combined effects of mass addition and nose bluntness on boundary-layer transition
    • May
    • Marvin, J., Akin, C.M., "Combined Effects of Mass Addition and Nose Bluntness on Boundary-Layer Transition", AIAA Journal, Vol. 8, No. 5, May 1970, pp. 857-863.
    • (1970) AIAA Journal , vol.8 , Issue.5 , pp. 857-863
    • Marvin, J.1    Akin, C.M.2
  • 16
    • 0040523507 scopus 로고
    • Experimental investigation of the downstream influence of stagnation-point mass transfer
    • Libby, P.A. and Cresci, R. J., "Experimental Investigation of the Downstream Influence of Stagnation-Point Mass Transfer", J. Aerospace Sci., Vol. 28. pp. 51-64, 1961.
    • (1961) J. Aerospace Sci. , vol.28 , pp. 51-64
    • Libby, P.A.1    Cresci, R.J.2
  • 18
    • 0004280576 scopus 로고
    • User's manual: Aerotherm chemical equilibrium computer program
    • Anon., Mountain View, CA, Aug.
    • Anon., "User's Manual: Aerotherm Chemical Equilibrium Computer Program," Report UM-81-11/ATD, Acurex Corp., Mountain View, CA, Aug. 1981.
    • (1981) Report UM-81-11/ATD, Acurex Corp.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.