Computation of Supersonic Flow over Flying Configurations

2

Hyperbolical Potential Boundary Value Problems of the Axial Disturbance Velocities of Outer Flow, at NSL’s Edge

Contents

2.1 Introduction

2.2 Basic equations

2.3 Full-linearized partial-differential equations of the flow over flattened, flying configurations

2.4 The characteristic hypersurfaces of the partial-differential equations of second order

2.5 The linearized pressure coefficient C_p on flying configurations

2.6 The linearized boundary value problems for flying configurations, at moderate angles of attack α

2.7 Definitions and properties of the thin and thick-symmetrical components of the thick, lifting flying configurations

2.8 The disturbance regions produced by a moving point in subsonic and supersonic flow

2.9 Disturbance regions ...