The expression of the aerodynamic force previously obtained in Chap. 12 is used to derive the Kutta-Jukowsky Theorem for a two-dimensional wing. The boundary condition and Kutta’s condition are also presented. The case of flat plate and its implications on the Doublet Lattice Method are discussed.
Theoretical Aerodynamic Modeling of Wings
Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity ; Kapitel : 18 ; 259-278
11.06.2024
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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