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Volumn 38, Issue 5, 2001, Pages 684-691

X-33 aerodynamic computations and comparisons with wind-tunnel data

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL METHODS; FINITE VOLUME METHOD; FLIGHT DYNAMICS; NAVIER STOKES EQUATIONS; SPACE RESEARCH; WIND TUNNELS;

EID: 0035439193     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3753     Document Type: Article
Times cited : (15)

References (25)
  • 2
    • 0003284355 scopus 로고    scopus 로고
    • X-33 reusable launch vehicle structural technologies
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    • (1996) AIAA Paper , vol.96 , Issue.4563
    • Cook, S.A.1
  • 14
    • 0002741308 scopus 로고
    • An upwind-biased, point-implicit algorithm for viscous, compressible perfect-gas flows
    • Feb.
    • (1990) NASA TP , vol.2953
    • Gnoffo, P.A.1
  • 22
    • 84959356593 scopus 로고    scopus 로고
    • Grid generation techniques utilizing the volume grid manipulator
    • June
    • (1998) AIAA Paper , vol.98 , Issue.3012
    • Alter, S.J.1
  • 23
    • 0002859431 scopus 로고    scopus 로고
    • The volume grid manipulator (VGM): A grid reusability tool
    • April
    • (1997) NASA CR , vol.4772
    • Alter, S.J.1
  • 24
    • 0003248544 scopus 로고
    • Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley research center: Aerothermodynamic facilities complex
    • June
    • (1995) AIAA Paper , vol.95 , Issue.2107
    • Micol, J.R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.