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Volumn , Issue , 2010, Pages

A "free" approach to Computational Aeroelasticity

Author keywords

[No Author keywords available]

Indexed keywords

BENCHMARKING; ELASTIC WAVES; FLUTTER (AERODYNAMICS); NUMERICAL METHODS;

EID: 78649820825     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-176     Document Type: Conference Paper
Times cited : (23)

References (24)
  • 3
    • 85040156458 scopus 로고
    • AGARD two-dimensional aeroelastic configurations
    • S. R. Bland, "AGARD two-dimensional aeroelastic configurations" , AGARD Advisory Report, 1979.
    • (1979) AGARD Advisory Report
    • Bland, S.R.1
  • 4
    • 78649886804 scopus 로고
    • AGARD standard aeroelastic configurations for dynamic response
    • E. Carson Yates, "AGARD standard aeroelastic configurations for dynamic response", NASA Technical Paper, 1987.
    • (1987) NASA Technical Paper
    • Yates, E.C.1
  • 6
    • 34248208696 scopus 로고    scopus 로고
    • Application of Navier-Stokes simulations for aeroelastic stability assesment in transonic regime
    • L. Cavagna, G. Quaranta and P. Mantegazza, "Application of Navier-Stokes simulations for aeroelastic stability assesment in transonic regime", Computers and Structures, 2007.
    • (2007) Computers and Structures
    • Cavagna, L.1    Quaranta, G.2    Mantegazza, P.3
  • 9
    • 1542603973 scopus 로고    scopus 로고
    • Aerodynamic shape optimization using a real number encoded genetic algorithm
    • T. H. Holst and T. H. Pullman, "Aerodynamic shape optimization using a real number encoded genetic algorithm", AIAA Technical Paper, 2001.
    • (2001) AIAA Technical Paper
    • Holst, T.H.1    Pullman, T.H.2
  • 15
    • 78649850560 scopus 로고
    • Experimental data base for computer program assessment: Pressure distribution measured in the RA 8 ft × 8 ft transonic wind tunnel on RAE wing A in combination with an aisymmetric body at Mach numbers of 0.4, 0.5 and 0.9
    • D. A. Treadgold, A.F. Jones and K. H. Wilson, "Experimental data base for computer program assessment: pressure distribution measured in the RA 8 ft × 8 ft transonic wind tunnel on RAE wing A in combination with an aisymmetric body at Mach numbers of 0.4, 0.5 and 0.9", AGARD Advisory Report, 1979.
    • (1979) AGARD Advisory Report
    • Treadgold, D.A.1    Jones, A.F.2    Wilson, K.H.3
  • 16
    • 78649852270 scopus 로고    scopus 로고
    • Various authors
    • Various authors, "Edge v.4.1 user's guide", www.foi.se/edge, 2005.
    • (2005) Edge V.4.1 User's Guide
  • 17
    • 28244482199 scopus 로고    scopus 로고
    • Various authors
    • Various authors, "Fluent v.6.2 user's guide", www.fluent.com, 2005.
    • (2005) Fluent V.6.2 User's Guide
  • 20
    • 78649813649 scopus 로고    scopus 로고
    • Various authors
    • Various authors, "Gnuplot v.4.2 user's guide", sourceforge.net/projects/gnuplot, 2007.
    • (2007) Gnuplot V.4.2 User's Guide
  • 23
    • 78649902626 scopus 로고    scopus 로고
    • Various authors
    • Various authors, "Salomé v.3.2.6 user's guide", www.salome-platform.org, 2008.
    • (2008) Salomé V.3.2.6 User's Guide


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.