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Volumn 34, Issue 1, 1997, Pages 8-15

Rarefied-flow transition regime orbiter aerodynamic acceleration flight measurements

Author keywords

[No Author keywords available]

Indexed keywords

ACCELEROMETERS; AERODYNAMICS; CALIBRATION; COMPUTER SIMULATION; FLIGHT DYNAMICS; HYPERSONIC AERODYNAMICS; HYPERSONIC FLOW; MONTE CARLO METHODS; TRANSITION FLOW; VELOCITY;

EID: 0030735823     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3183     Document Type: Article
Times cited : (11)

References (18)
  • 6
    • 0022098203 scopus 로고
    • The Shuttle Orbiter High Resolution Accelerometer Package Experiment: Preliminary Flight Results
    • Blanchard, R. C., and Rutherford, J. F., "The Shuttle Orbiter High Resolution Accelerometer Package Experiment: Preliminary Flight Results," Journal of Spacecraft and Rockets, Vol. 22, No. 4, 1985, pp. 474-480.
    • (1985) Journal of Spacecraft and Rockets , vol.22 , Issue.4 , pp. 474-480
    • Blanchard, R.C.1    Rutherford, J.F.2
  • 8
    • 84889505220 scopus 로고
    • Space Div., Rockwell International, CA STS 85-0118 CHG 3, Downey, CA, Sept.
    • Anon., "Operational Aerodynamic Design Data Book," Space Div., Rockwell International, CA STS 85-0118 CHG 3, Downey, CA, Sept. 1991.
    • (1991) Operational Aerodynamic Design Data Book
  • 13
  • 14
    • 0028422495 scopus 로고
    • Navier-Stokes Simulations of Orbiter Aerodynamic Characteristics Including Pitch Trim and Bodyflap
    • Weilmuenster, K. J., Gnoffo, P. A., and Greene, F. A., "Navier-Stokes Simulations of Orbiter Aerodynamic Characteristics Including Pitch Trim and Bodyflap," Journal of Spacecraft and Rockets, Vol. 31, No. 3, 1994, pp. 355-366.
    • (1994) Journal of Spacecraft and Rockets , vol.31 , Issue.3 , pp. 355-366
    • Weilmuenster, K.J.1    Gnoffo, P.A.2    Greene, F.A.3
  • 15
    • 0003703360 scopus 로고
    • National Oceanic and Atmospheric Administration, NASA, and U.S. Air Force, Oct.
    • Anon., U.S. Standard Atmosphere, 1976, National Oceanic and Atmospheric Administration, NASA, and U.S. Air Force, Oct. 1976.
    • (1976) U.S. Standard Atmosphere, 1976
  • 16
    • 84964217697 scopus 로고
    • Orbiter Rarefied-Flow Aerodynamics and Upper-Atmosphere Density Flight Measurements
    • (Williamsburg, VA), edited by D. A. Throckmorton, NASA CP 3248, April
    • Blanchard, R. C., Nicholson, J. Y., Larman, K. T., and Ozoroski, T. A., "Orbiter Rarefied-Flow Aerodynamics and Upper-Atmosphere Density Flight Measurements," Proceedings of Orbiter Experiment (OEX) Aerothermodynamics Symposium (Williamsburg, VA), edited by D. A. Throckmorton, NASA CP 3248, April 1995, pp. 553-575.
    • (1995) Proceedings of Orbiter Experiment (OEX) Aerothermodynamics Symposium , pp. 553-575
    • Blanchard, R.C.1    Nicholson, J.Y.2    Larman, K.T.3    Ozoroski, T.A.4
  • 17
    • 0028544870 scopus 로고
    • Aerodynamics of the Shuttle Orbiter at High Altitudes
    • Rault, D. F. G., "Aerodynamics of the Shuttle Orbiter at High Altitudes," Journal of Spacecraft and Rockets, Vol. 31, No. 6, 1994, pp. 944-952.
    • (1994) Journal of Spacecraft and Rockets , vol.31 , Issue.6 , pp. 944-952
    • Rault, D.F.G.1
  • 18
    • 0010281724 scopus 로고    scopus 로고
    • DSMC Grid Methodologies for Computing Low-Density Hypersonic Flows about Reusable Launch Vehicles
    • June
    • Wilmoth, R. G., LeBeau, G. J., and Carlson, A. B., "DSMC Grid Methodologies for Computing Low-Density Hypersonic Flows About Reusable Launch Vehicles," AIAA Paper 96-1812, June 1996.
    • (1996) AIAA Paper 96-1812
    • Wilmoth, R.G.1    LeBeau, G.J.2    Carlson, A.B.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.