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Volumn 16, Issue 1, 2002, Pages 94-100

Unified calculation of hypersonic flowfield for a reentry vehicle

Author keywords

[No Author keywords available]

Indexed keywords

ABLATION; AERODYNAMIC HEATING; COMPUTATIONAL FLUID DYNAMICS; ITERATIVE METHODS; PROBLEM SOLVING; REENTRY; TURBULENCE;

EID: 0036098034     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/2.6656     Document Type: Article
Times cited : (41)

References (29)
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    • Milos, F.S.1
  • 3
    • 0006058878 scopus 로고    scopus 로고
    • Heatshielding problems of planetary entry, a review
    • July
    • (1999) AIAA Paper , vol.99 , Issue.3415
    • Park, C.1
  • 5
    • 0021372893 scopus 로고
    • Injection-induced turbulence in stagnation point boundary layers
    • (1984) AIAA Journal , vol.22 , Issue.2 , pp. 219-225
    • Park, C.1
  • 11
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  • 20
    • 0006126444 scopus 로고
    • Jan.
    • (1994) AIAA Paper , vol.94 , Issue.83
  • 24
    • 0006096003 scopus 로고    scopus 로고
    • Nonequilibrium flow computation for the space shuttle nose using unstructured meshes
    • June
    • (1997) AIAA Paper , vol.97 , Issue.2548
    • Niizuma, K.1    Sawada, K.2
  • 28


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.