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Volumn , Issue , 2001, Pages

Implementation of a re-entry CFD toolbox in the gesared flight simulator

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894442706     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (11)
  • 7
    • 0021386091 scopus 로고
    • Hypersonic Mach number and Real gas Effect on Space Shuttle Orbiter Aerodynamics
    • Maus, J. R., et al., Hypersonic Mach number and Real gas Effect on Space Shuttle Orbiter Aerodynamics, Journal of Spacecraft and Rockets, vol. 21, nO.2, March-April 1984, pp 136-141
    • (1984) Journal of Spacecraft and Rockets , vol.21 , Issue.2 , pp. 136-141
    • Maus, J.R.1
  • 10
    • 0016896841 scopus 로고
    • Boundary Layer Stability and Transition
    • Reshotko, Eli: Boundary Layer Stability and Transition in Annual Review of fluid Mechanics, vol. 8, 1976, pp 311-349
    • (1976) Annual Review of Fluid Mechanics , vol.8 , pp. 311-349
    • Reshotko, E.1
  • 11
    • 0019476840 scopus 로고
    • Approximate Convective-Heating Equations for Hypersonic Flows
    • Zoby, E.V., J.N. Moss, and K. Sutton: Approximate Convective-Heating Equations for Hypersonic Flows Journal of Spacecraft and Rockets, vol. 18, no. 1, January-February 1981, pp 64-70
    • (1981) Journal of Spacecraft and Rockets , vol.18 , Issue.1 , pp. 64-70
    • Zoby, E.V.1    Moss, J.N.2    Sutton, K.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.