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- W2389747584 abstract "A simple nonlinear wing theory for the low-aspect-ratio rectangular flat plate with large angle of attack in incompressible flow is developed. The plate is replaced by a finite number of horseshoe vortex lines which are located along the chord of the plate and which are of different strength. The free parts of the vortex lines make an angle θ with the plate. For the solution of the problem an iterative procedure is applied. The angle θ is initially assumed to be one half of the angle of attack and the first approximate values for the strength of the vortex lines are computed. By application of the Helmholtz principle at the side edges of the plate, the second approximate value for the angle θ is determined. By repeating this calculation, the second approximate values for the strength of the vortex lines and then the aerodynamic coefficients of the plate are obtained. A few examples are calculated and the theoretical results are compared with the experimental ones. It is shown that for low-aspect-ratio rectangular plates this theory agrees very well with the experiments." @default.
- W2389747584 created "2016-06-24" @default.
- W2389747584 creator A5016434270 @default.
- W2389747584 date "1964-01-01" @default.
- W2389747584 modified "2023-09-23" @default.
- W2389747584 title "A SIMPLE METHOD FOR CALCULATING THE AERODYNAMIC CHARACTERISTICS OF LOWASPECT-RATIO RECTANGULAR FLAT PLATES WITH LARGE ANGLE OF ATTACK IN INCOMPRESSIBLE FLOW" @default.
- W2389747584 hasPublicationYear "1964" @default.
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