The Kutta conditionKutta condition in all physical and mathematical flow models defined in Sect. 10.1007/978-3-662-61328-3_1 is generally understood as appearing at acute edges of aerodynamic surfaces. That can be the “zero thickness” trailing edge of a large Aspect ratiolarge aspect-ratio wing or the “sharp” leading edge of a delta wing. Usually it is assumed that the flow leaves the trailing edge in bisector direction.
About the Kutta Condition
Separated and Vortical Flow in Aircraft Wing Aerodynamics ; Kapitel : 6 ; 127-145
05.10.2020
19 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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