Computation of Supersonic Flow over Flying Configurations

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Zonal, Spectral Solutions for the Three-Dimensional, Compressible Navier–Stokes Layer

Contents

1.1 Introduction

1.2 Three-dimensional, partial-differential equations of compressible Navier-Stokes layer (NSL)

1.3 The spectral variable and the spectral forms of the velocity’s components and of the physical entities

1.4 The first and second derivatives of the velocity’s components

1.5 The implicit and explicit forms of the boundary conditions at the NSL’s edge

1.6 The dependence of the density function R versus the spectral velocity, inside the NSL

1.7 Dependence of absolute temperature T versus the spectral velocity, inside the NSL

1.8 The scalar forms of the NSL’s impulse’s partial-differential equations and their equivalent quadratical algebraic ...