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Volumn , Issue , 2003, Pages

Optimization of long-endurance airfoils

Author keywords

Inverse design; Maximum endurance factors; Optimization

Indexed keywords

AIRFOILS; LIFT; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; OPTIMIZATION; REYNOLDS NUMBER;

EID: 85067316853     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3500     Document Type: Conference Paper
Times cited : (11)

References (10)
  • 1
    • 84897715434 scopus 로고    scopus 로고
    • ERAST project, NASA Website
    • "ERAST" project, NASA Website.
  • 2
    • 0030836840 scopus 로고    scopus 로고
    • High-Lift Low Reynolds Number Airfoil Design
    • Selig, M.S., and Guglielmo, J.J., High-Lift Low Reynolds Number Airfoil Design, Journal of Aircraft, Vol. 34, No. 1, 1997.
    • (1997) Journal of Aircraft , vol.34 , Issue.1
    • Selig, M.S.1    Guglielmo, J.J.2
  • 6
    • 85088724110 scopus 로고    scopus 로고
    • Towards Efficient Aerodynamic Shape Optimization Based on the Navier-Stokes Equations
    • Nemec, M., and Zingg, D.W., Towards Efficient Aerodynamic Shape Optimization Based on the Navier-Stokes Equations, AIAA 2001-2532, 2001.
    • (2001) AIAA 2001-2532
    • Nemec, M.1    Zingg, D.W.2
  • 7
    • 0036603032 scopus 로고    scopus 로고
    • Newton-Krylov Algorithm for Aerodynamic Design using the Navier-Stokes Equations
    • Nemec, M., and Zingg, D.W., Newton-Krylov Algorithm for Aerodynamic Design using the Navier-Stokes Equations, AIAA Journal, Vol. 40, No. 6, 2002.
    • (2002) AIAA Journal , vol.40 , Issue.6
    • Nemec, M.1    Zingg, D.W.2
  • 8
    • 84897698230 scopus 로고
    • An Iterative Procedure for Three-Dimensional Transonic Wing design by the Integral Equation Method
    • Takanashi, S., An Iterative Procedure for Three-Dimensional Transonic Wing design by the Integral Equation Method, AIAA-85-1595, 1985.
    • (1985) AIAA-85-1595
    • Takanashi, S.1
  • 10
    • 84888776017 scopus 로고
    • Newton Solution of Coupled Viscous-Inviscid Multi-element Airfoil Flow
    • Drela, M., Newton Solution of Coupled Viscous-Inviscid Multi-element Airfoil Flow, AIAA 90-1470, 1990.
    • (1990) AIAA 90-1470
    • Drela, M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.