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Volumn 22, Issue 5, 2005, Pages 393-398

High-order accurate scheme WCNS-E-5 applied to body heat transfer distributions

Author keywords

High order accurate scheme; Navier Stokes equations; Weighted compact nonlinear scheme

Indexed keywords

NAVIER STOKES EQUATIONS; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; VISCOUS FLOW;

EID: 26644469087     PISSN: 1001246X     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (6)

References (12)
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  • 2
    • 0028448330 scopus 로고
    • Nonlinearly stable compact schemes for shock calculations
    • Cockburn B, Shu C W. Nonlinearly stable compact schemes for shock calculations [J]. SIAM J Numer Anal, 1994, 31: 607-630.
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  • 3
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    • Chinese source
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    • Chinese source
  • 5
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    • Compact high-order accurate nonlinear schemes
    • Deng X G, Maekawa H. Compact high-order accurate nonlinear schemes [J]. J Comp Phys, 1997, 130: 77-91.
    • (1997) J Comp Phys , vol.130 , pp. 77-91
    • Deng, X.G.1    Maekawa, H.2
  • 6
    • 4344718753 scopus 로고    scopus 로고
    • Weighted compact high-order nonlinear schemes for the Euler equations
    • AIAA paper, 97-1941
    • Deng Xiaogang, Mao Meiliang. Weighted compact high-order nonlinear schemes for the Euler equations [R]. AIAA paper, 97-1941, 1997.
    • (1997)
    • Deng, X.1    Mao, M.2
  • 7
    • 0008978420 scopus 로고    scopus 로고
    • Developing high-order accurate nonlinear schemes
    • Deng Xiaogang, Zhang Hanxin. Developing high-order accurate nonlinear schemes [J]. J Comp Phys, 2000, 165: 22-44.
    • (2000) J Comp Phys , vol.165 , pp. 22-44
    • Deng, X.1    Zhang, H.2
  • 8
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    • The convergence rate for difference approximations to mixed initial boundary value problems
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  • 11
    • 3142602380 scopus 로고    scopus 로고
    • Effects of angle of attack and bluntness on laminar heating-rating distributions of a 15° cone at a Mach number of 10.6
    • NASA TND-5450
    • Cleary J W. Effects of angle of attack and bluntness on laminar heating-rating distributions of a 15° cone at a Mach number of 10.6 [R]. NASA TND-5450.
    • Cleary, J.W.1
  • 12
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    • Application of the multigrid solution technique to hypersonic entry vehicles
    • AIAA paper 93-2721
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.