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Computation of Supersonic Flow over Flying Configurations by Adriana Nastase

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8

Computation of the Friction Drag Coefficients of the Flying Configurations

8.1. Introduction

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 [1] and [2] 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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