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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Steady Incompressible Ideal Flow and Modeling of Finite Wings


    Contributors:


    Publication date :

    2024-06-11


    Size :

    27 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English