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Volumn 38, Issue 5, 2001, Pages 658-669

X-33 computational aeroheating predictions and comparisons with experimental data

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC HEATING; BOUNDARY LAYERS; COMPUTATION THEORY; ELECTRIC POWER SYSTEM PROTECTION; FINITE VOLUME METHOD; LAMINAR FLOW; NAVIER STOKES EQUATIONS; SPACE RESEARCH; TURBULENT FLOW; WIND TUNNELS;

EID: 0035438996     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3751     Document Type: Article
Times cited : (32)

References (35)
  • 2
    • 0003284355 scopus 로고    scopus 로고
    • X-33 reusable launch vehicle structural technologies
    • Nov.
    • (1996) AIAA Paper , vol.96 , Issue.4563
    • Cook, S.A.1
  • 23
    • 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
  • 24
    • 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


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.