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Volumn , Issue , 2008, Pages

Heating augmentation in laminar flow due to heat-shield cavities on the Project Orion CEV

Author keywords

[No Author keywords available]

Indexed keywords

ADDITIONAL HEATING; AEROHEATING; CAVITY DIMENSION; CAVITY HEATING; EXPERIMENTAL STUDIES; LAMINAR CONDITION; MARS SCIENCE LABORATORY; PHOSPHOR THERMOGRAPHY;

EID: 77958474505     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (17)
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  • 3
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    • March-April
    • Liechty, D. S., Hollis, B. R., and Edquist, K. T., "Mars Science Laboratory Experimental Aerothermodynamics with Effects of Cavities and Control Surfaces," Journal of Spacecraft and Rockets, Vol. 43, No. 2, March-April 2006, pp. 340-353.
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    • Liechty, D.S.1    Hollis, B.R.2    Edquist, K.T.3
  • 4
    • 33646706820 scopus 로고    scopus 로고
    • Transition due to heat-shield cavities on a mars entry vehicle
    • March-April
    • Hollis, B. R., and Liechty, D. S., "Transition Due to Heat-Shield Cavities on a Mars Entry Vehicle," Journal of Spacecraft and Rockets, Vol. 43, No. 2, March-April 2006, pp. 354-366.
    • (2006) Journal of Spacecraft and Rockets , vol.43 , Issue.2 , pp. 354-366
    • Hollis, B.R.1    Liechty, D.S.2
  • 5
    • 78649486290 scopus 로고    scopus 로고
    • Correlations for boundary-layer transition on mars science laboratory entry vehicle due to heat-shield cavities
    • June
    • Hollis, B. R. and Liechty, D. S., "Correlations for Boundary-Layer Transition on Mars Science Laboratory Entry Vehicle Due to Heat-Shield Cavities," NASA TP-2008-215317, June 2008.
    • (2008) NASA TP-2008-215317
    • Hollis, B.R.1    Liechty, D.S.2
  • 7
    • 77958456042 scopus 로고    scopus 로고
    • Aerothermodynamic testing of protuberances and penetrations on the NASA crew exploration vehicle heat shield
    • Reno, NV, January 7-10
    • Liechty, D. S., "Aerothermodynamic Testing of Protuberances and Penetrations on the NASA Crew Exploration Vehicle Heat Shield," AIAA Paper 2008-1240, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 7-10, 2008.
    • (2008) th AIAA Aerospace Sciences Meeting and Exhibit
    • Liechty, D.S.1
  • 9
    • 0002724964 scopus 로고
    • Surface temperature/heat transfer measurement using a quantitative phosphor thermography system
    • January
    • Buck, G. M., "Surface Temperature/Heat Transfer Measurement Using a Quantitative Phosphor Thermography System," AIAA Paper 91-0064, January 1991.
    • (1991) AIAA Paper 91-0064
    • Buck, G.M.1
  • 10
    • 0033100191 scopus 로고    scopus 로고
    • Global aeroheating wind-tunnel measurements using improved two-color phosphor thermography methods
    • March-April
    • Merski, N. R., "Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Thermography Methods, Journal of Spacecraft and Rockets, Vol. 36, No. 2, pp. 160-170, March-April 1999.
    • (1999) Journal of Spacecraft and Rockets , vol.36 , Issue.2 , pp. 160-170
    • Merski, N.R.1
  • 11
    • 0002887728 scopus 로고
    • Theory of stagnation point heat transfer in dissociated air
    • February
    • 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, February 1958.
    • (1958) Journal of Aeronautical Sciences , vol.25 , Issue.2 , pp. 73-85
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  • 13
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    • An upwind-biased, point-implicit algorithm for viscous, compressible perfect-gas flows
    • February
    • Gnoffo, P. A., "An Upwind-Biased, Point-Implicit Algorithm for Viscous, Compressible Perfect-Gas Flows," NASA TP-2953, February 1990.
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  • 14
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    • April
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  • 15
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  • 16
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  • 17
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.