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Volumn 31, Issue 1, 2002, Pages 25-40

Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; DRAG; LIFT;

EID: 0036028022     PISSN: 00457930     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7930(01)00014-7     Document Type: Article
Times cited : (10)

References (26)
  • 7
    • 0000170864 scopus 로고
    • The approximate arithmetical solution by finite differences of physical problems involving differential equations, with an application to the stresses in a masonry dam
    • (1910) Trans Roy Soc London Ser A , vol.210 , pp. 307-357
    • Richardson, L.F.1
  • 17
    • 0024144053 scopus 로고
    • Viscous transonic airfoil workshop compendium of results
    • (1988) J Aircraft , vol.25 , pp. 1073-1087
    • Holst, T.L.1
  • 22
    • 0022162768 scopus 로고
    • A mathematically simple turbulence closure model for attached and separated turbulent boundary layers
    • (1985) AIAA J , vol.23 , Issue.11 , pp. 1684-1692
    • Johnson, D.A.1    King, L.S.2
  • 24


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.