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Volumn 14, Issue 3, 2000, Pages 421-434

Ablation onset in unsteady hypersonic flow about nose tip with cavity

Author keywords

[No Author keywords available]

Indexed keywords

ABLATION; COMPUTATIONAL METHODS; COMPUTER SIMULATION; HEAT CONDUCTION; HEATING; MATHEMATICAL MODELS; UNSTEADY FLOW; WIND TUNNELS;

EID: 0034224893     PISSN: 08878722     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.6540     Document Type: Article
Times cited : (28)

References (20)
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    • Engblom, W. A., "Numerical Investigation of Hypersonic Flow over a Forward-Facing Cavity," Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics, Univ. of Texas, Austin, TX, Aug. 1996, pp. 20-29, 36, 41, 122-125, 128-143.
    • (1996) Numerical Investigation of Hypersonic Flow over a Forward-facing Cavity , pp. 20-29
    • Engblom, W.A.1
  • 3
    • 85001975497 scopus 로고
    • A preliminary investigation of the Helmholtz resonator concept for heat flux reduction
    • July
    • Yuceil, B., Dolling, D. S., and Wilson, D., "A preliminary Investigation of the Helmholtz Resonator Concept for Heat Flux Reduction," AIAA Paper 93-2742, July 1993.
    • (1993) AIAA Paper 93-2742
    • Yuceil, B.1    Dolling, D.S.2    Wilson, D.3
  • 4
    • 0030145589 scopus 로고    scopus 로고
    • Experimental and numerical study of hypersonic forward-facing cavity flow'
    • Engblom, W. A., Yuceil, B., Goldstein, D. B., and Dolling, D. S., "Experimental and Numerical Study of Hypersonic Forward-Facing Cavity Flow'," Journal of Spacecraft and Rockets, Vol. 33, No. 3, 1996, pp. 353-359.
    • (1996) Journal of Spacecraft and Rockets , vol.33 , Issue.3 , pp. 353-359
    • Engblom, W.A.1    Yuceil, B.2    Goldstein, D.B.3    Dolling, D.S.4
  • 9
    • 49049151571 scopus 로고
    • Flux vector splitting of the inviscid gasdynamic equations with applications to finite-difference methods
    • Steger, J. L., and Warming, R. F., "Flux Vector Splitting of the Inviscid Gasdynamic Equations with Applications to Finite-Difference Methods," Journal of Computational Physics. Vol. 40, No. 2, 1981, pp. 263-293.
    • (1981) Journal of Computational Physics , vol.40 , Issue.2 , pp. 263-293
    • Steger, J.L.1    Warming, R.F.2
  • 12
    • 0010932986 scopus 로고
    • Sandia National Labs., SAND88-1326, Albuquerque, NM, June
    • Blacker, T. D., "FASTQ Users Manual Version 1.2," Sandia National Labs., SAND88-1326, Albuquerque, NM, June 1988.
    • (1988) FASTQ Users Manual Version 1.2
    • Blacker, T.D.1
  • 13
    • 0343532457 scopus 로고    scopus 로고
    • IR imaging and shock visualization of flow over a blunt body with a nose cavity
    • Jan.
    • Yuceil, B., and Dolling, D. S., "IR Imaging and Shock Visualization of Flow over a Blunt Body with a Nose Cavity," AIAA Paper 96-0232, Jan. 1996.
    • (1996) AIAA Paper 96-0232
    • Yuceil, B.1    Dolling, D.S.2
  • 14
    • 0003812713 scopus 로고
    • Clarendon, Oxford
    • Hobbs, P. V., Ice Physics, Clarendon, Oxford, 1974, p. 348.
    • (1974) Ice Physics , pp. 348
    • Hobbs, P.V.1
  • 17
    • 0342662273 scopus 로고
    • Full scale ablation testing of candidate hypervelocity nose tip materials
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    • Reinecke, W. G., and Guillot, M. J., "Full Scale Ablation Testing of Candidate Hypervelocity Nose Tip Materials," Proceedings of the 15th International Symposium on Ballistics, Vol. 2, Secretariat 15th International Symposium on Ballistics, Tel Aviv, 1995, pp. 81-88.
    • (1995) Proceedings of the 15th International Symposium on Ballistics , vol.2 , pp. 81-88
    • Reinecke, W.G.1    Guillot, M.J.2
  • 18
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    • Tip survivability and performance on hypervelocity projectiles
    • American Defense Preparedness Association, Arlington, VA
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    • (1993) Proceedings of the 14th International Symposium on Ballistics , vol.1 , pp. 575-588
    • Reinecke, W.G.1    Sherman, M.2
  • 19
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    • Theory of stagnation point heat transfer in dissociated air
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.