The Doublet Lattice Method requires the aerodynamic steady solution that is based on the Vortex Lattice Method (VLM). How this solution is obtained is discussed in this chapter. Moreover, the Prandtl-Glauert compressibility correction is also introduced to extend the validity to steady compressible fluid.
Steady Incompressible Ideal Flow and Modeling of Finite Wings
Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity ; Kapitel : 19 ; 279-305
11.06.2024
27 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Symmetry conditions , Control point , Panel , Normalwash , Load point , Vortex Lattice Method , Aerodynamic influence matrix , Prandtl-Glauert compressibility correction Mechanical Engineering , Physics and Astronomy , Structural Materials , Mechanical Statics and Structures , Aerospace Technology and Astronautics , Engineering
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