The aerodynamic modeling of wings performed by using vortices requires the calculation of the resulting aerodynamic forces. This chapter provides the theoretical background that is required to achieve that goal for wings placed in the three-dimensional space.
The Aerodynamic Force for the Steady Incompressible Ideal Flow
Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity ; Chapter : 12 ; 161-172
2024-06-11
12 pages
Article/Chapter (Book)
Electronic Resource
English
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