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 ; Chapter : 20 ; 309-330
2024-06-11
22 pages
Article/Chapter (Book)
Electronic Resource
English
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