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 ; Chapter : 19 ; 279-305
2024-06-11
27 pages
Article/Chapter (Book)
Electronic Resource
English
Vortex Lattice Method , Aerodynamic influence matrix , Normalwash , Symmetry conditions , Prandtl-Glauert compressibility correction , Load point , Control point , Panel Engineering , Aerospace Technology and Astronautics , Mechanical Engineering , Mechanical Statics and Structures , Structural Materials , Physics and Astronomy
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