Simplified transonic integral equations for lifting profiles and wings
The basic small perturbation integral equations for steady inviscid transonic flow past a thin cambered profile at small incidence have been simplified here using Oswatitsch substitution for the velocity field in terms of that on the profile axis. The resulting equations contain only one-dimensional singular integrals.
steady inviscid transonic flow past a thin cambered profile at small incidence
scientific article; zbMATH DE number 3890957
scientific article