Computation of Supersonic Flow over Flying Configurations

9

Inviscid and Viscous Aerodynamical Global Optimal Design

Contents

9.1 Introduction

9.2 The optimum-optimorum theory

9.3 Inviscid aerodynamical global optimal design, via optimum-optimorum theory

9.4 Inviscid aerodynamic global optimal design of delta wing model ADELA, via optimum-optimorum theory

9.5 Inviscid aerodynamic global optimal design of fully-integrated wing/fuselage models FADET I and FADET II

9.6 The iterative optimum-optimorum theory and the viscous aerodynamical optimal design

9.7 Proposal for a fully-optimized and fully-integrated Catamaran STA

9.8 Conclusions

9.1. Introduction

In this chapter is presented a further application of the author’s original, zonal, spectral solutions for the compressible stationary Navier-Stokes ...