Design of airfoil with high ratio of lift over drag

Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

Volumn 22, Issue 4, 2004, Pages 410-415

  Liu, Zhou ^a   Zhu, Zi Qiang ^a   Fu, Hong Yan ^a   Wu, Zong Cheng ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

High ratio of lift over drag; Parameterized function method; Powell method

Indexed keywords

DESIGN; DRAG; LIFT; NAVIER STOKES EQUATIONS; OPTIMIZATION; RUNGE KUTTA METHODS; VISCOUS FLOW;

BALDMIN LOMAX MODEL; PARAMETERIZED FUNCTION METHOD; POWELL METHOD; RUNGE KUTTA TIME STEPPING METHOD;

AIRFOILS;

EID: 14344260870     PISSN: 02581825     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

1. LIOU M S. Progress towards an improved CFD method: AUSM+[R]. AIAA95-1701.
2. BALDWIN B S, LOMAX H. Thin layer approximation algebraic model for separated turbulent flow[R]. AIAA78-257, 1978.
3. POWELL M J D. An efficient method for finding the minimum of a function of several variables without calculation derivatives[J]. Computer Journal, 1964, 7(2): 155-162.
4. HICKS R M, HENNE P A. Wing design by numerical optimization[R]. AIAA 77-1247.
5. SOBIECZKY H. Parametric airfoils and wings[J]. Note on Numerical Fluid Mechanics. 1998. 71-88. Vieweg.