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Volumn , Issue , 2005, Pages

Computational aerothermodynamic assessment of space shuttle Orbiter tile damage - open cavities

Author keywords

[No Author keywords available]

Indexed keywords

DAMAGE SCENARIOS; FLIGHT CONDITIONS; FLIGHT SIMULATION; RATE OF INCREASE; REFERENCE VALUES; SPACE SHUTTLE ORBITER; TRAJECTORY POINTS; WIND-TUNNEL SIMULATION;

EID: 33947272649     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (15)

References (22)
  • 1
    • 84884763353 scopus 로고    scopus 로고
    • Prediction of STS-107 Hypervelocity Flow Fields about the Shuttle Orbiter with Various Wing Leading Edge Damage
    • Colorado Springs, Colorado
    • Pulsonetti, M. V., Thompson, R. A, and Alter, S. J., "Prediction of STS-107 Hypervelocity Flow Fields about the Shuttle Orbiter with Various Wing Leading Edge Damage, " JANNAF Conference, Colorado Springs, Colorado, 2003
    • (2003) JANNAF Conference
    • Pulsonetti, M.V.1    Thompson, R.A.2    Alter, S.J.3
  • 5
    • 84884806967 scopus 로고    scopus 로고
    • Experimental and Computational Investigation of Cavity Flow Simulating Debris Damage to Thermal Protection System Tiles
    • Colorado Springs, Colorado
    • Everhardt, J. L., Bey, K. S., Wood, W. A., and Pulsonetti, M. V., "Experimental and Computational Investigation of Cavity Flow Simulating Debris Damage to Thermal Protection System Tiles, " JANNAF Conference, Colorado Springs, Colorado, 2003
    • (2003) JANNAF Conference
    • Everhardt, J.L.1    Bey, K.S.2    Wood, W.A.3    Pulsonetti, M.V.4
  • 8
    • 0027626039 scopus 로고
    • Solution Strategy for Three-Dimensional Configurations at Hypersonic Speeds
    • July-August
    • Weilmuenster, K.J. and Gnoffo, P.A., "Solution Strategy for Three-Dimensional Configurations at Hypersonic Speeds, " Journal of Spacecraft an Rockets, Vol. 30, No. 4, July-August 1993, pp. 385-394
    • (1993) Journal of Spacecraft an Rockets , vol.30 , Issue.4 , pp. 385-394
    • Weilmuenster, K.J.1    Gnoffo, P.A.2
  • 10
    • 2942757053 scopus 로고
    • Approximate Riemann Solvers, Parameter Vectors and Difference Schemes
    • Roe, P. L., "Approximate Riemann Solvers, Parameter Vectors and Difference Schemes, " Journal of Computational Physics, Vol. 43, No. 2, 1981, pp. 357-372.
    • (1981) Journal of Computational Physics , vol.43 , Issue.2 , pp. 357-372
    • Roe, P.L.1
  • 11
    • 40749159424 scopus 로고
    • High Resolution Schemes for Hyperbolic Conservation Laws
    • Harten, A., "High Resolution Schemes for Hyperbolic Conservation Laws, " Journal of Computational Physics, Vol. 49, No. 3, 1983, pp. 357-393.
    • (1983) Journal of Computational Physics , vol.49 , Issue.3 , pp. 357-393
    • Harten, A.1
  • 13
    • 0002887728 scopus 로고
    • Theory of Stagnation Point Heat Transfer in Dissociated Air
    • Feb
    • Fay, J.A., and Riddell, F.R., "Theory of Stagnation Point Heat Transfer in Dissociated Air, " Journal of Aeronautical Sciences, Vol. 25, No. 2, pp. 73-85, Feb. 1958.
    • (1958) Journal of Aeronautical Sciences , vol.25 , Issue.2 , pp. 73-85
    • Fay, J.A.1    Riddell, F.R.2
  • 19
    • 0021873741 scopus 로고
    • The Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow
    • AIAA-85-0971, Williamsburg, Virginia, June
    • th Thermophysics Conference, Williamsburg, Virginia, June 1985
    • (1985) th Thermophysics Conference
    • Nestler, D.E.1
  • 22
    • 85007683104 scopus 로고
    • Experimental Investigation of Separated Flow over a Cavity at Hypersonic Speed
    • June
    • Hahn, M., "Experimental Investigation of Separated Flow over a Cavity at Hypersonic Speed, " AIAA Journal, Vol. 7, No. 7, June 1969, pp. 1092-1098
    • (1969) AIAA Journal , vol.7 , Issue.7 , pp. 1092-1098
    • Hahn, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.