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Contents
2.3 Development and Influence Mechanism of Boundary
Layer Near Airfoil Surface
97
2.4 Low-Speed Flow Around Wing
108
2.5 Basic Theory of Compressible Flow
117
2.6 Solution of Compressible Flow
135
2.7 Hypersonic Aerodynamics
138
2.8 Principle of Aeroacoustics
144
2.9 Stall Characteristics of Low-Speed Airfoil and Wing
153
2.10 Interaction Between Shock Wave and Boundary Layer
in Supersonic Flow
161
2.11 The Leading Role of Aerodynamics in the Development
of Modern Aircraft
171
3 Hydrodynamics
175
3.1 Development of Hydrodynamics
175
3.2
Liquid Motion
180
3.2.1 Ideal Liquid Motion
180
3.2.2 Viscous Liquid Motion
180
3.2.3 Cavitation and Cavitation Erosion
181
3.2.4 Multiphase Flow
181
3.2.5 Non-newtonian Fluid Flow
182
3.2.6 Non Pressure Flow (Open Flow)
183
3.2.7 Pressure Flow
183
3.2.8 Flow Induced Vibration (Hydroelastic
Problem)
184
3.3 One-Dimensional Flow Theory and Mechanical
Energy Loss
184
3.3.1 Theory of One-Dimensional Flow
184
3.3.2 Mechanical Energy Loss
187
3.4 Steady Flow Along a Pressure Pipeline
192
3.4.1 Simple Pipe Flow
192
3.4.2 Water Pump System
194
3.4.3 Water Turbine System
196
3.5 Steady Flow in Open Channel
197
3.5.1 Overview
197
3.5.2 Steady Uniform Flow in Open Channel
199
3.5.3 Steady Nonuniform Gradually Varied Flow
201
3.5.4 Water Surface Curves for the Steady Gradually
Varied Flow
206
3.5.5 Rapidly Varied Flow in the Open Channel
208