论文信息 - Slender wing in ground effect - 字舞流文

Slender wing in ground effect

Determination analytique du coefficient de portance d'une aile mince en effet de sol. Comparaison avec les resultats numeriques obtenus par la methode des panneaux

S. S. Dodbele | A. Plotkin | S. Dodbele | A. Plotkin

[1] R. Agarwal,et al. Euler calculation for flow over a wing in ground effect , 1986 .

[2] E. O. Tuck,et al. Steady flow and static stability of airfoils in extreme ground effect , 1981 .

[3] N. Rott,et al. Generalizations of the Inversion Formula of Thin Airfoil Theory , 1954 .

[4] A. Plotkin. Thickness and Camber Effects in Slender Wing Theory , 1983 .

[5] Allen Plotkin,et al. Lifting-line solution for a symmetrical thin wing in ground effect , 1986 .

[6] J. N. Newman. Analysis of small-aspect-ratio lifting surfaces in ground effect , 1982, Journal of Fluid Mechanics.

[7] B. Maskew. PROGRAM VSAERO: A computer program for calculating the non-linear aerodynamic characteristics of arbitrary configurations: User's manual , 1982 .

[8] Joseph Katz,et al. Calculation of the Aerodynamic Forces on Automotive Lifting Surfaces , 1985 .

[9] A. Plotkin,et al. Thickness-Induced Lift on a Thin Airfoil in Ground Effect , 1981 .

[10] M. Hashiguchi. Computational Study of Aerodynamic Behavior of a Car Configuration , 1987 .