Preface |
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xi | |
Acknowledgment |
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xiii | |
Author |
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xv | |
Notation |
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xvii | |
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1 | (14) |
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1 | (2) |
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Function analysis (derivatives) |
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3 | (3) |
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4 | (2) |
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Derivatives of functions of multi-variables |
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6 | (4) |
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6 | (1) |
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7 | (2) |
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9 | (1) |
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10 | (3) |
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11 | (1) |
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12 | (1) |
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13 | (2) |
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2 Fundamental Principles of Aerodynamics (Subsonic) |
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15 | (24) |
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15 | (2) |
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17 | (11) |
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21 | (1) |
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Applications of Bernoulli's Equation |
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22 | (1) |
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Venturi Tube (Flowrate Meter) |
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22 | (2) |
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24 | (1) |
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Lift Produced by a Subsonic Aerofoil |
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25 | (1) |
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26 | (2) |
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First Law of Thermodynamics |
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28 | (1) |
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29 | (5) |
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29 | (1) |
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30 | (1) |
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31 | (1) |
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Isochoric (Isovolumetric) Process |
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31 | (2) |
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33 | (1) |
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34 | (3) |
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36 | (1) |
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37 | (2) |
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3 Viscous Flow and Boundary Layer |
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39 | (22) |
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39 | (3) |
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Effect of Pressure and Temperature on Viscosity |
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40 | (2) |
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42 | (2) |
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Reynolds Number and Regimes of Viscous Flow |
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44 | (3) |
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45 | (1) |
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45 | (2) |
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47 | (13) |
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Structure of the Boundary Layer |
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48 | (2) |
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Viscous Flow of Boundary Layer |
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50 | (1) |
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Speed Profile within the Boundary Layer |
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50 | (2) |
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Viscous Friction (Skin Drag) |
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52 | (2) |
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Boundary-Layer Separation over a Curved Surface (Stall) |
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54 | (3) |
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Form Drag - Separation Drag |
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57 | (3) |
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60 | (1) |
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4 Aerodynamic Forces - Subsonic Flight |
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61 | (32) |
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Geometric Features of Aerofoils |
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61 | (4) |
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62 | (2) |
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64 | (1) |
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65 | (9) |
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66 | (1) |
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67 | (2) |
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Circulation Theory of Lift |
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69 | (5) |
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74 | (10) |
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75 | (2) |
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77 | (2) |
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79 | (1) |
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80 | (1) |
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80 | (1) |
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81 | (2) |
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83 | (1) |
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Features of Aerofoil on Aerodynamic Forces |
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84 | (8) |
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84 | (2) |
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86 | (1) |
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87 | (1) |
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88 | (1) |
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Features to Delay/Prevent Boundary Layer Separation |
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88 | (3) |
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91 | (1) |
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92 | (1) |
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92 | (1) |
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93 | (30) |
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93 | (4) |
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93 | (1) |
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93 | (1) |
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94 | (2) |
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96 | (1) |
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96 | (1) |
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Pitch Moment and Pitch Moment Coefficient |
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97 | (6) |
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99 | (1) |
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Calculation of Aerodynamic Center |
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99 | (4) |
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103 | (5) |
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Effects on Longitudinal Stability |
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103 | (1) |
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104 | (1) |
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104 | (1) |
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105 | (1) |
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106 | (1) |
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106 | (1) |
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Longitudinal Stability Diagram |
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107 | (1) |
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108 | (6) |
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Factors on Lateral Stability |
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109 | (1) |
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109 | (1) |
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110 | (1) |
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111 | (1) |
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111 | (1) |
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112 | (1) |
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Lateral Stability Diagram |
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112 | (2) |
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114 | (5) |
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Factors on Directional Stability |
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115 | (1) |
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115 | (1) |
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116 | (1) |
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117 | (1) |
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117 | (1) |
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Directional Stability Diagram |
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117 | (2) |
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Lateral and Directional Stability (Dynamic) |
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119 | (1) |
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119 | (1) |
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119 | (1) |
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Design Requirements for Lateral and Directional Stability |
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120 | (1) |
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Longitudinal Dynamic Stability |
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120 | (1) |
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120 | (1) |
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121 | (1) |
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121 | (2) |
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6 Speed of Sound and Mach Number |
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123 | (14) |
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123 | (3) |
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126 | (5) |
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127 | (1) |
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128 | (1) |
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129 | (2) |
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131 | (1) |
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131 | (3) |
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131 | (1) |
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High Subsonic and Low Transonic Flight |
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132 | (1) |
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133 | (1) |
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134 | (2) |
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136 | (1) |
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137 | (22) |
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Compressible 1-D Airflow System |
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137 | (7) |
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137 | (1) |
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Momentum (Euler) Equation |
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138 | (1) |
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138 | (1) |
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Ideal Gas Law (State Equation of Gas) |
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138 | (1) |
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138 | (4) |
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142 | (2) |
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Compressible Airflow with a Variable Area of Flow Path |
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144 | (6) |
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Converging-Diverging Nozzle |
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147 | (3) |
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150 | (6) |
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150 | (1) |
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Air Properties Before and after a Normal Shockwave |
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150 | (6) |
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156 | (2) |
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158 | (1) |
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8 Aerodynamics of Transonic Aerofoils |
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159 | (16) |
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159 | (4) |
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Structure of Shockwave on Aerofoil |
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159 | (2) |
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Movement of Shockwave on Aerofoil |
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161 | (2) |
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Effective Critical Mach Number |
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163 | (1) |
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Changes of CP, CL, and CD on a Transonic Aerofoil |
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163 | (5) |
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163 | (1) |
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164 | (1) |
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164 | (1) |
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164 | (1) |
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Changes of CP, CL, and CD between Mcrit to Mdet |
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165 | (3) |
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168 | (1) |
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Shockwaves on Control Surfaces |
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169 | (5) |
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169 | (1) |
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169 | (3) |
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172 | (1) |
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172 | (2) |
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174 | (1) |
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9 Transonic Flight and Aerofoils |
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175 | (18) |
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175 | (4) |
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176 | (1) |
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177 | (1) |
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Effects on Buffet Boundary |
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178 | (1) |
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179 | (1) |
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180 | (3) |
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181 | (1) |
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182 | (1) |
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182 | (1) |
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183 | (1) |
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183 | (7) |
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Low Thickness to Chord Ratio tic |
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183 | (2) |
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185 | (1) |
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186 | (3) |
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Devices to Delay Shock Stall |
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189 | (1) |
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189 | (1) |
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190 | (1) |
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190 | (1) |
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190 | (1) |
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191 | (2) |
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193 | (20) |
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Two Examples of Reversible and Irreversible Adiabatic Processes (Supersonic) |
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193 | (2) |
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193 | (1) |
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194 | (1) |
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195 | (10) |
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Air Properties Before and After an Oblique Shockwave |
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196 | (4) |
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200 | (5) |
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205 | (6) |
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Air Properties before and after Expansion Waves |
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206 | (2) |
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208 | (1) |
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209 | (2) |
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211 | (2) |
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11 Introduction of Supersonic Flight |
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213 | (18) |
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Supersonic Flow over Aerofoil |
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213 | (9) |
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214 | (1) |
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214 | (2) |
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216 | (3) |
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219 | (3) |
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222 | (2) |
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Boundary Layer in Supersonic Flow |
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222 | (1) |
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Drag of Supersonic Flight |
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223 | (1) |
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Supersonic Wings and Planforms |
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224 | (4) |
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224 | (1) |
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225 | (1) |
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225 | (1) |
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226 | (1) |
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Body Shapes of Supersonic Airplanes |
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227 | (1) |
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228 | (2) |
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230 | (1) |
Appendix I List of Derivatives |
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231 | (2) |
Appendix II 6-B-M Diagram |
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233 | (2) |
Appendix III Prandtl-Meyer Function |
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235 | (2) |
Appendix IV Answers to Exercises |
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237 | (6) |
References |
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243 | (2) |
Index |
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245 | |