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Volumn , Issue , 2002, Pages

Vehicle design of a sharp CTV concept using a virtual flight rapid integration test environment

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; CONCEPTUAL DESIGN; FLIGHT SIMULATORS; INTEGRATION; NASA; NUMERICAL METHODS; OPTIMIZATION; QUALITY CONTROL; TESTING; VEHICLES; VIRTUAL REALITY; WIND STRESS;

EID: 85086614680     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4881     Document Type: Conference Paper
Times cited : (5)

References (19)
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  • 2
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  • 3
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  • 5
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    • First Flight Demonstration of a Sharp Ultra- High Temperature Ceramic Nosetip
    • December
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  • 6
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  • 7
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    • st Century Space Transportation System Design Approach: HL-20 Personnel Launch System
    • September- October
    • Stone, H. W. and Piland, W. M., 21st Century Space Transportation System Design Approach: HL-20 Personnel Launch System, AIAA Journal of SpaceCraft and Rockets, 30(5):521-528, September- October 1993.
    • (1993) AIAA Journal of SpaceCraft and Rockets , vol.30 , Issue.5 , pp. 521-528
    • Stone, H.W.1    Piland, W.M.2
  • 9
    • 1842721928 scopus 로고    scopus 로고
    • Robust and Efficient Cartesian Mesh Generation for Component-Based Geometry
    • January
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  • 10
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    • Baker, T.J.1    Vassberg, J.C.2
  • 11
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  • 13
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  • 14
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.