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Volumn 36, Issue 2, 1999, Pages 171-178

X-34 experimental aeroheating at Mach 6 and 10

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC HEATING; AIRCRAFT MODELS; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; HEAT TRANSFER; HYPERSONIC AERODYNAMICS; REYNOLDS NUMBER; SHOCK WAVES; SURFACES; TRAJECTORIES; WIND TUNNELS;

EID: 0033098796     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3447     Document Type: Article
Times cited : (29)

References (25)
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  • 4
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    • Riley, C. J., Kleb, W. L., and Alter, S. J., "Aeroheating Predictions for X-34 Using an Inviscid Boundary-Layer Method," Journal of Spacecraft and Rockets, Vol. 36, No. 2, 1999, pp. 206-215.
    • (1999) Journal of Spacecraft and Rockets , vol.36 , Issue.2 , pp. 206-215
    • Riley, C.J.1    Kleb, W.L.2    Alter, S.J.3
  • 5
    • 0033101228 scopus 로고    scopus 로고
    • Engineering aerothermal analysis for X-34 thermal protection system design
    • Wurster, K. E., Riley, C. J., and Zoby, E. V., "Engineering Aerothermal Analysis for X-34 Thermal Protection System Design," Journal of Spacecraft and Rockets. Vol. 36, No. 2, 1999, pp. 216-228.
    • (1999) Journal of Spacecraft and Rockets , vol.36 , Issue.2 , pp. 216-228
    • Wurster, K.E.1    Riley, C.J.2    Zoby, E.V.3
  • 6
    • 0033100191 scopus 로고    scopus 로고
    • Global aeroheating wind-tunnel measurements using improved two-color phosphor thermography method
    • Merski, N. R., "Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Thermography Method," Journal of Spacecraft and Rockets, Vol. 36, No. 2, 1999, pp. 160-170; also "Reduction and Analysis of Phosphor Thermography Data with the IHEAT Software Package," AIAA Paper 98-0712, Jan. 1998.
    • (1999) Journal of Spacecraft and Rockets , vol.36 , Issue.2 , pp. 160-170
    • Merski, N.R.1
  • 7
    • 0033100191 scopus 로고    scopus 로고
    • AIAA Paper 98-0712, Jan.
    • Merski, N. R., "Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Thermography Method," Journal of Spacecraft and Rockets, Vol. 36, No. 2, 1999, pp. 160-170; also "Reduction and Analysis of Phosphor Thermography Data with the IHEAT Software Package," AIAA Paper 98-0712, Jan. 1998.
    • (1998) Reduction and Analysis of Phosphor Thermography Data with the IHEAT Software Package
  • 14
    • 0029368516 scopus 로고
    • Aerothermodynamic measurement and prediction for a modified orbiter at mach 6 and 10 in air
    • Micol, J. R., "Aerothermodynamic Measurement and Prediction for a Modified Orbiter at Mach 6 and 10 in Air," Journal of Spacecraft and Rockets, Vol. 32, No. 5, 1995, pp. 737-748.
    • (1995) Journal of Spacecraft and Rockets , vol.32 , Issue.5 , pp. 737-748
    • Micol, J.R.1
  • 15
    • 0032075307 scopus 로고    scopus 로고
    • Shuttle orbiter experimental boundary-layer transition results with isolated roughness
    • Berry, S. A., Bouslog, S. A., Brauckmann, G. J., and Caram, J. M., "Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness," Journal of Spacecraft and Rockets, Vol. 35, No. 3, 1998, pp. 241-248.
    • (1998) Journal of Spacecraft and Rockets , vol.35 , Issue.3 , pp. 241-248
    • Berry, S.A.1    Bouslog, S.A.2    Brauckmann, G.J.3    Caram, J.M.4
  • 16
    • 0002887728 scopus 로고
    • Theory of stagnation point heat transfer in dissociated air
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  • 17
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  • 20
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  • 22
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    • Navier-Stokes heating calculations for Benchmark thermal protection system sizing
    • Olynick, D. R., and Henline, W. D., "Navier-Stokes Heating Calculations for Benchmark Thermal Protection System Sizing," Journal of Spacecraft and Rockets, Vol. 33, No. 6, 1996, pp. 807-814.
    • (1996) Journal of Spacecraft and Rockets , vol.33 , Issue.6 , pp. 807-814
    • Olynick, D.R.1    Henline, W.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.