Computation of the Friction Drag Coefficients of the Flying Configurations
The starting point of the computation of the friction drag coefficient are the partial differential equations (PDEs) of the Navier-Stokes layer (NSL), given in  and  without any simplification.
In this chapter is presented a further application of the original, zonal, spectral solutions for the compressible stationary NSL over flattened flying configurations (FCs) presented in Chap. 1 and in ...
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