메뉴 건너뛰기




Volumn , Issue , 2009, Pages

Heating augmentation due to compression pad cavities on the Project Orion CEV heat shield

Author keywords

[No Author keywords available]

Indexed keywords

AEROHEATING; BOUNDARY-LAYER TRANSITION; CAVITY DIMENSION; EXPERIMENTAL STUDIES; HEAT SHIELDS; PHOSPHOR THERMOGRAPHY;

EID: 77958464759     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (22)
  • 2
    • 77958474505 scopus 로고    scopus 로고
    • Augmentation in laminar flow due to heat-shield cavities on the project orion CEV
    • Heating, Honolulu, HI, August 18-21, AIAA Paper 2008-6558
    • Hollis, B. R., "Heating Augmentation in Laminar Flow Due to Heat-Shield Cavities on the Project Orion CEV," AIAA Paper 2008-6558, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Honolulu, HI, August 18-21, 2008.
    • (2008) AIAA Atmospheric Flight Mechanics Conference and Exhibit
    • Hollis, B.R.1
  • 3
    • 77958456042 scopus 로고    scopus 로고
    • Aerothermodynamic testing of protuberances and penetrations on the nasa crew exploration vehicle shield
    • AIAA Paper 2008-1240, Reno, NV, January 7-10
    • Liechty, D. S., "Aerothermodynamic Testing of Protuberances and Penetrations on the NASA Crew Exploration Vehicle Shield," AIAA Paper 2008-1240, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 7-10, 2008.
    • (2008) 46th AIAA Aerospace Sciences Meeting and Exhibit
    • Liechty, D.S.1
  • 4
    • 85088341564 scopus 로고    scopus 로고
    • Rapid model fabrication and testing for aerospace vehicles
    • AIAA Paper 2000-0826, Reno, NV, January 10-13
    • Buck, G. M., "Rapid Model Fabrication and Testing for Aerospace Vehicles," AIAA Paper 2000-0826, 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2000.
    • (2000) 38th AIAA Aerospace Sciences Meeting and Exhibit
    • Buck, G.M.1
  • 5
    • 84982318849 scopus 로고    scopus 로고
    • Langley aerothermodynamic facilities complex: Enhancements and testing capabilities
    • AIAA Paper 98-0147, Reno, NV, January 12-15
    • Micol, J. R. "Langley Aerothermodynamic Facilities Complex: Enhancements and Testing Capabilities," AIAA Paper 98-0147, 36th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 12-15, 1998.
    • (1998) 36th AIAA Aerospace Sciences Meeting and Exhibit
    • Micol, J.R.1
  • 7
    • 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
  • 8
    • 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
    • Fay, J.A.1    Riddell, F.R.2
  • 14
    • 33646673838 scopus 로고    scopus 로고
    • Mars science laboratory experimental aerothermodynamics with effects of cavities and control surfaces
    • March-April
    • Liechty, D. S., and Hollis, B. R., "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.
    • (2006) Journal of Spacecraft and Rockets , vol.43 , Issue.2 , pp. 340-353
    • Liechty, D.S.1    Hollis, B.R.2
  • 15
    • 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
  • 17
    • 84894548756 scopus 로고    scopus 로고
    • Aerothermodynamic environment definition for the genesis sample return capsule
    • AIAA Paper 2001-2889, Anaheim, CA, June 11-14
    • Cheatwood, F. M., Merski, N. R., Riley, C. J., and Mitcheltree, R. A., "Aerothermodynamic Environment Definition for the Genesis Sample Return Capsule," AIAA Paper 2001-2889, 35th AIAA Thermophysics Conference, Anaheim, CA, June 11-14, 2001.
    • (2001) 35th AIAA Thermophysics Conference
    • Cheatwood, F.M.1    Merski, N.R.2    Riley, C.J.3    Mitcheltree, R.A.4
  • 18
    • 0001325343 scopus 로고
    • An investigation of separated flow- Part I, The pressure field
    • June
    • Charwat, A. F., Roos, J. N., Dewy, C. F., and Hitz, J. A., "An Investigation of Separated Flow - Part I, The Pressure Field," Journal of the Aerospace Sciences, Vol. 28, No. 6, June 1961, pp. 457-470.
    • (1961) Journal of the Aerospace Sciences , vol.28 , Issue.6 , pp. 457-470
    • Charwat, A.F.1    Roos, J.N.2    Dewy, C.F.3    Hitz, J.A.4
  • 19
    • 0001325343 scopus 로고
    • An investigation of separated flow- Part I, flow in the cavity and heat transfer
    • July
    • Charwat, A. F., Dewey, C. F., Roos, J. N., and Hitz, J. A., "An Investigation of Separated Flow - Part I, Flow in the Cavity and Heat Transfer," Journal of the Aerospace Sciences, Vol. 28, No. 7, July 1961, pp. 513-527.
    • (1961) Journal of the Aerospace Sciences , vol.28 , Issue.7 , pp. 513-527
    • Charwat, A.F.1    Dewey, C.F.2    Roos, J.N.3    Hitz, J.A.4
  • 20
    • 42949091822 scopus 로고    scopus 로고
    • Discrete roughness transition for hypersonic flight vehicles
    • March-April
    • Berry, S. A., and Horvath, T. J., "Discrete Roughness Transition for Hypersonic Flight Vehicles," Journal of Spacecraft and Rockets, Vol. 45, No. 2, March-April 2008, pp. 21-227.
    • (2008) Journal of Spacecraft and Rockets , vol.45 , Issue.2 , pp. 21-227
    • Berry, S.A.1    Horvath, T.J.2
  • 21
    • 77958498422 scopus 로고    scopus 로고
    • Supersonic/hypersonic laminar heating correlations for rectangular and impact-induced open and closed cavities
    • AIAA Paper 2008-1283, Reno, NV, January 7-10
    • Everhart, J. L., "Supersonic/Hypersonic Laminar Heating Correlations for Rectangular and Impact-Induced Open and Closed Cavities," AIAA Paper 2008-1283, 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 7-10, 2008.
    • (2008) 46th AIAA Aerospace Sciences Meeting and Exhibit
    • Everhart, J.L.1
  • 22
    • 78549287152 scopus 로고    scopus 로고
    • Turbulent supersonic/hypersonic heating correlations for open and closed cavities
    • AIAA Paper 2009-1400, Orlando, FL, January 5-8
    • Everhart, J. L., "Turbulent Supersonic/Hypersonic Heating Correlations for Open and Closed Cavities," AIAA Paper 2009-1400, 47th AIAA Aerospace Sciences Meeting, Orlando, FL, January 5-8, 2009.
    • (2009) 47th AIAA Aerospace Sciences Meeting
    • Everhart, J.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.