The unsteady aerodynamics is usually presented in terms of a relatively complicated integral equation where the unknown pressure jump appears within an integral over the wing system. This concept is introduced in this chapter.
Two-Dimensional Unsteady Incompressible Flow
Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity ; Kapitel : 20 ; 309-330
11.06.2024
22 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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