메뉴 건너뛰기




Volumn , Issue , 2004, Pages 10915-10932

Experimental aerothermodynamics in support of the Columbia accident investigation

Author keywords

[No Author keywords available]

Indexed keywords

ACCIDENTS; AERODYNAMICS; BOUNDARY LAYERS; COMPUTER SIMULATION; FUSELAGES; HEAT TRANSFER; HEATING; HYPERSONIC AERODYNAMICS; LANDING GEAR (AIRCRAFT); MAPPING; NUMERICAL METHODS; REYNOLDS NUMBER; SPACE SHUTTLES; THERMODYNAMICS; WIND TUNNELS; WINGS;

EID: 2942739133     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1387     Document Type: Conference Paper
Times cited : (17)

References (24)
  • 1
    • 2942717851 scopus 로고    scopus 로고
    • August
    • CAIB Final Report. Vol. I, August, 2003.
    • (2003) CAIB Final Report , vol.1
  • 2
    • 2942753053 scopus 로고    scopus 로고
    • Appendix D.7, August
    • CAIB Final Report. Vol. II, Appendix D.7, August, 2003.
    • (2003) CAIB Final Report , vol.2
  • 3
    • 0037463350 scopus 로고    scopus 로고
    • Rough wing + debris = A fatal combination
    • Feb., 24
    • Covault, C., "Rough Wing + Debris = A Fatal Combination," Aviation Week & Space Technology, Vol. 158, No. 8, pp. 20-22, Feb., 24, 2003.
    • (2003) Aviation Week & Space Technology , vol.158 , Issue.8 , pp. 20-22
    • Covault, C.1
  • 5
    • 0037437180 scopus 로고    scopus 로고
    • Connecting the dots
    • April, 14
    • Morring, Frank, Jr., "Connecting the Dots" Aviation Week & Space Technology, Vol. 158, No. 15, pp. 30-31, April, 14, 2003.
    • (2003) Aviation Week & Space Technology , vol.158 , Issue.15 , pp. 30-31
    • Morring Jr., F.1
  • 6
    • 0037459987 scopus 로고    scopus 로고
    • Columbia probe shifts
    • April, 21
    • Covault, C., "Columbia Probe Shifts," Aviation Week & Space Technology, Vol. 158, No. 16, pp. 29-30, April, 21, 2003.
    • (2003) Aviation Week & Space Technology , vol.158 , Issue.16 , pp. 29-30
    • Covault, C.1
  • 7
    • 85002522460 scopus 로고
    • Experimental investigation of gamma effects on heat transfer to a 0.006 scale shuttle orbiter at mach 6
    • Miller, C. G., "Experimental Investigation of Gamma Effects on Heat Transfer to a 0.006 Scale Shuttle Orbiter at Mach 6," AIAA Paper 82-0826, 1982.
    • (1982) AIAA Paper , vol.82 , Issue.826
    • Miller, C.G.1
  • 8
    • 0029370656 scopus 로고
    • Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly
    • Brauckmann, G. J., Paulson, J. W., and Weilmuenster, J. K., "Experimental and Computational Analysis of Shuttle Orbiter Hypersonic Trim Anomaly," Journal of Spacecraft and Rockets, Vol. 32, No. 5, pp. 758-764, 1995.
    • (1995) Journal of Spacecraft and Rockets , vol.32 , Issue.5 , pp. 758-764
    • Brauckmann, G.J.1    Paulson, J.W.2    Weilmuenster, J.K.3
  • 10
    • 2942723422 scopus 로고
    • Orbiter leeside surface aeroheating environment characterization
    • NASA CP 3248, Part 2
    • Throckmorton, D. A., "Orbiter Leeside Surface Aeroheating Environment Characterization," Orbiter Experiments (OEX) Aerothermodynamics Symposium, NASA CP 3248, Part 2, pp. 811-822, 1995.
    • (1995) Orbiter Experiments (OEX) Aerothermodynamics Symposium , pp. 811-822
    • Throckmorton, D.A.1
  • 11
    • 2942747388 scopus 로고
    • Orbiter pre STS-1 aeroheating design data base development methodology: Comparison of wind tunnel and flight test data
    • NASA CP 3248, Part 2
    • Haney, J. W., "Orbiter Pre STS-1 Aeroheating Design Data Base Development Methodology: Comparison of Wind Tunnel and Flight Test Data," Orbiter Experiments (OEX) Aerothermodynamics Symposium, NASA CP 3248, Part 2, pp. 607-676, 1995.
    • (1995) Orbiter Experiments (OEX) Aerothermodynamics Symposium , pp. 607-676
    • Haney, J.W.1
  • 12
    • 7544227691 scopus 로고
    • Use of tetrafluoromethane to simulate real-gas effects on the hypersonic aerodynamics of blunt vehicles
    • Jones, R. A., and Hunt, J. L., "Use of Tetrafluoromethane to Simulate Real-Gas Effects on the Hypersonic Aerodynamics of Blunt Vehicles,", NASA TR 312, 1969.
    • (1969) NASA TR , vol.312
    • Jones, R.A.1    Hunt, J.L.2
  • 13
    • 85086615500 scopus 로고    scopus 로고
    • Discrete roughness effects on shuttle orbiter at mach 6
    • Berry, S. A., Hamilton, H. H., "Discrete Roughness Effects on Shuttle Orbiter at Mach 6," AIAA Paper 2002-2744, 2002.
    • (2002) AIAA Paper , vol.2002 , Issue.2744
    • Berry, S.A.1    Hamilton, H.H.2
  • 14
    • 84862371262 scopus 로고
    • "An Investment Ceramic Slip-Casting Technique for Net-Form, Precision, Detailed Casting of Ceramic Models," U. S. Patent 5,266,252
    • Buck, G. M., and Vasquez, P., "An Investment Ceramic Slip-Casting Technique for Net-Form, Precision, Detailed Casting of Ceramic Models," U. S. Patent 5,266,252, 1993.
    • (1993)
    • Buck, G.M.1    Vasquez, P.2
  • 15
    • 2342583113 scopus 로고    scopus 로고
    • Rapid model fabrication and testing for aerospace vehicles
    • Buck, G. M., "Rapid Model Fabrication and Testing for Aerospace Vehicles," AIAA Paper 2000-0826, 2000.
    • (2000) AIAA Paper , vol.2000 , Issue.826
    • Buck, G.M.1
  • 16
    • 2342539427 scopus 로고
    • Automated thermal mapping techniques using chromatic image analysis
    • Buck, G. M., "Automated Thermal Mapping Techniques Using Chromatic Image Analysis," NASA TM 101554, 1989.
    • (1989) NASA TM 101554
    • Buck, G.M.1
  • 17
    • 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, pp. 160-170, 1998.
    • (1998) Journal of Spacecraft and Rockets , vol.36 , Issue.2 , pp. 160-170
    • Merski, N.R.1
  • 18
    • 84896692994 scopus 로고    scopus 로고
    • Finite volume numerical methods for aeroheating rate calculations from infrared thermographic data
    • Daryabeigi, K., Berry, S. A., Horvath, T. J., and Nowak, R. J., "Finite Volume Numerical Methods for Aeroheating Rate Calculations From Infrared Thermographic Data," AIAA Paper 2003-3634, 2003.
    • (2003) AIAA Paper , vol.2003 , Issue.3634
    • Daryabeigi, K.1    Berry, S.A.2    Horvath, T.J.3    Nowak, R.J.4
  • 19
    • 0002824511 scopus 로고
    • Langley hypersonic aerodynamic/aerothermodynamic testing capabilities - Present and future
    • Miller, C. G., "Langley Hypersonic Aerodynamic/Aerothermodynamic Testing Capabilities - Present and Future," AIAA Paper 90-1376, 1990.
    • (1990) AIAA Paper , vol.90 , Issue.1376
    • Miller, C.G.1
  • 21
    • 84982318636 scopus 로고    scopus 로고
    • Reduction and analysis of phosphor thermography data with the iheat software package
    • Merski, N. R., "Reduction and Analysis of Phosphor Thermography Data With the IHEAT Software Package," AIAA Paper 98-0712, 1998.
    • (1998) AIAA Paper , vol.98 , Issue.712
    • Merski, N.R.1
  • 22
    • 2942747387 scopus 로고    scopus 로고
    • Space shuttle orbiter aerodynamics induced by asymmetric boundary-layer transition
    • An, M. Y., Wang, K. C., Campbell, C. H., and Pelley, R. L., "Space Shuttle Orbiter Aerodynamics Induced by Asymmetric Boundary-Layer Transition," AIAA Paper 96-0712, 1996.
    • (1996) AIAA Paper , vol.96 , Issue.712
    • An, M.Y.1    Wang, K.C.2    Campbell, C.H.3    Pelley, R.L.4
  • 24
    • 23544434512 scopus 로고
    • A study of leeside flow field heat transfer on shuttle orbiter configurations
    • Baranowski, L. C., and Kipp, H. W., "A Study of Leeside Flow Field Heat Transfer On Shuttle Orbiter Configurations," NASA Contract NAS1-16839, 1983.
    • (1983) NASA Contract , vol.NAS1-16839
    • Baranowski, L.C.1    Kipp, H.W.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.