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Volumn 39, Issue 10, 2001, Pages 1884-1892

Validation of computed high-lift flows with significant wind-tunnel effects

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; WIND TUNNELS; WINGS;

EID: 0035475733     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1203     Document Type: Article
Times cited : (36)

References (30)
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  • 12
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  • 13
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  • 14
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    • Numerical study of a trapezoidal wing high-lift configuration
    • Society of Automotive Engineers, Paper 1999-01-5559, Oct.
    • (1999)
    • Nash, S.M.1    Rogers, S.E.2
  • 17
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    • Experimental investigation of a simplified 3D high lift configuration in support of CFD validation
    • AIAA Paper 2000-4217, Aug.
    • (2000)
    • Johnson, P.1    Jones, K.M.2    Madson, M.3
  • 19
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    • Taft, J.1
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    • Parallelism and OVERFLOW
    • NASA Advanced Supercomputing Facility, TR NAS-98-013, NASA Ames Research Center, Moffett Field, CA, Oct.
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    • Jespersen, D.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.