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Algorithm Issues and Challenges Associated with the Development of Robust CFD Codes |
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1 | (20) |
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1 | (1) |
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Algorithm Issues Related to the Solution of the Navier-Stokes Equations |
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2 | (17) |
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Grid Adaption and Error Estimation |
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3 | (3) |
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6 | (6) |
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12 | (4) |
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Domain Decomposition and Linear Solver |
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16 | (3) |
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19 | (2) |
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19 | (2) |
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Flight Path Optimization at Constant Altitude |
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21 | (12) |
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21 | (2) |
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23 | (1) |
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24 | (2) |
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Fanjet Specific Fuel Consumption |
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26 | (2) |
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28 | (3) |
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Conclusions and Discussion |
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31 | (2) |
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32 | (1) |
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A Survey on the Newton Problem of Optimal Profiles |
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33 | (16) |
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33 | (4) |
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Radially Symmetric Profiles |
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37 | (3) |
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40 | (9) |
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47 | (2) |
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Innovative Rotor Blade Design Code |
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49 | (26) |
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50 | (1) |
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Helicopter's Aeromechanics Outlines |
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51 | (5) |
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Helicopter's Rotor Mathematical Model Features and Aeromechanics Codes Worldwide Status |
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56 | (1) |
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AW Aeromechanics Code GYROX II |
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57 | (11) |
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58 | (1) |
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Rotor Hub Modelling Features |
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59 | (2) |
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61 | (1) |
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Rotor Blade Structural Modelling Features |
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62 | (1) |
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63 | (3) |
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66 | (1) |
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Operational Main Features and Output Data |
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67 | (1) |
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68 | (5) |
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73 | (2) |
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73 | (1) |
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74 | (1) |
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Fields of Extremals and Sufficient Conditions for the Simplest Problem of the Calculus of Variations in n- Variables |
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75 | (16) |
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75 | (1) |
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Notations and the Problem Definition |
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76 | (2) |
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78 | (2) |
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80 | (4) |
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Sufficient Conditions for Optimality |
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84 | (4) |
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88 | (3) |
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88 | (3) |
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A Framework for Aerodynamic Shape Optimization |
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91 | (16) |
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91 | (1) |
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Adjoint-Based Sensitivity Analysis |
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92 | (1) |
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93 | (7) |
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94 | (2) |
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96 | (2) |
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98 | (1) |
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99 | (1) |
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99 | (1) |
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100 | (5) |
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RAE2822 at M∞ = 0.73 and α = 2° |
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100 | (1) |
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NACA64A410 at M∞ = 0.75 and α = 0° |
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101 | (1) |
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NACA0012 at M∞ = 1.5 and α = 2° |
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102 | (1) |
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ONERA-M6 wing at M∞ = 0.84 and α = 3.06° |
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103 | (2) |
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105 | (2) |
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106 | (1) |
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Optimal Motions of Multibody Systems in Resistive Media |
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107 | (20) |
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107 | (1) |
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108 | (2) |
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110 | (1) |
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110 | (2) |
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Piecewise Linear Resistance |
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112 | (1) |
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113 | (1) |
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Dry Friction: Velocity-Control Motion |
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114 | (6) |
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Dry Friction: Acceleration Control Motion |
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120 | (4) |
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124 | (1) |
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124 | (1) |
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125 | (2) |
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125 | (2) |
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Instationary Heat-Constrained Trajectory Optimization of a Hypersonic Space Vehicle by ODE-PDE-Constrained Optimal Control |
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127 | (18) |
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128 | (2) |
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Trajectory Optimization Problems with Active Cooling |
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130 | (4) |
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Trajectory Optimization Problem with an Instationary Heat Constraint |
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134 | (6) |
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140 | (5) |
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142 | (3) |
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Variational Approaches to Fracture |
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145 | (18) |
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Fracture as a Minimum Problem |
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145 | (2) |
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147 | (1) |
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Energy Barriers and Local Minima |
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148 | (3) |
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Barenblatt's Regularization |
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151 | (2) |
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153 | (1) |
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154 | (3) |
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From Surface to Bulk Regularization |
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157 | (6) |
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161 | (2) |
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On the Problem of Synchronization of Identical Dynamical Systems: The Huygens's Clocks |
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163 | (20) |
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163 | (3) |
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A Model for the Synchronization of the Two Pendulum Clocks |
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166 | (2) |
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168 | (1) |
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Synchronization of Two Pendulum Clocks with Equal Parameters |
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169 | (9) |
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Synchronization of Two Pendulum Clocks with Different Parameters Robustness |
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178 | (1) |
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179 | (4) |
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180 | (3) |
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Best Wing System: An Exact Solution of the Prandtl's Problem |
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183 | (30) |
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183 | (1) |
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The Induced Drag for Lifting Multiwing Systems |
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184 | (3) |
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The Problem of Minimum Induced Drag in a Box Wing |
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187 | (9) |
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Case A: Elliptical Circulations on the Horizontal Wings and Zero on the Vertical Ones |
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191 | (1) |
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Case B: Constant Circulations on the Horizontal Wings and Unknown on the Vertical Ones |
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192 | (2) |
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194 | (2) |
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The Optimum Lift Distribution Along the Vertical Wings |
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196 | (1) |
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197 | (16) |
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199 | (14) |
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Numerical Simulation of the Dynamics of Boats by a Variational Inequality Approach |
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213 | (16) |
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213 | (1) |
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A Vanational Approach to the Floating Body Problem |
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214 | (9) |
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Characteristic Treatment of the Time Derivative |
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218 | (1) |
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Enforcing the Constraint in the Hydrostatic Step |
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219 | (1) |
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The Model for the Dynamics of a Rowing Scull |
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220 | (3) |
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More Realistic Boundary Conditions |
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223 | (1) |
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The Interaction Between the Boat and the Water |
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223 | (1) |
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224 | (5) |
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Sinking and Pitching Motions |
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224 | (1) |
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Reproducing Mean Motion Wave Pattern |
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225 | (1) |
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An Example with the Full Dynamics |
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226 | (1) |
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226 | (1) |
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227 | (2) |
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Concepts of Active Noise Reduction Employed in High Noise Level Aircraft Cockpits |
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229 | (14) |
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Passive Versus Active Noise Reduction |
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230 | (1) |
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Active Noise Cancellation |
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230 | (4) |
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Active Structural/Acoustic Control (ASAC) |
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234 | (3) |
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237 | (1) |
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An Aviation Communication Headset Prototype with Digital Adaptive Noise Reduction |
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238 | (2) |
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240 | (3) |
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240 | (3) |
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Lekhnitskii's Formalism for Stress Concentrations Around Irregularities in Anisotropic Plates: Solutions for Arbitrary Boundary Conditions |
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243 | (24) |
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243 | (2) |
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245 | (1) |
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246 | (1) |
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Stress, Strain, and Displacements Formulation |
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247 | (1) |
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Formulation of Boundary Conditions |
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248 | (2) |
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248 | (1) |
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249 | (1) |
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250 | (3) |
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Series Representation of the Boundary Conditions |
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250 | (1) |
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Transformation into a Single Variable |
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251 | (2) |
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Boundary Conditions Evaluation |
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253 | (6) |
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253 | (1) |
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254 | (2) |
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256 | (3) |
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Evaluation of Stresses and Displacements |
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259 | (2) |
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261 | (3) |
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264 | (3) |
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265 | (2) |
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Best Initial Conditions for the Rendezvous Maneuver |
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267 | (24) |
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268 | (1) |
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269 | (2) |
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271 | (5) |
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Multiple-Subarc Equations |
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272 | (1) |
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273 | (1) |
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274 | (1) |
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274 | (1) |
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275 | (1) |
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276 | (1) |
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276 | (1) |
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277 | (3) |
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280 | (7) |
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282 | (5) |
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287 | (4) |
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288 | (3) |
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Commercial Aircraft Design for Reduced Noise and Environmental Impact |
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291 | (22) |
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292 | (1) |
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Simple Emission Trade-Off Study |
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292 | (3) |
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292 | (1) |
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293 | (1) |
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Local Air Quality Cost (LAQ) |
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293 | (1) |
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Annual Fuel Costs Fro Baseline Aircraft |
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294 | (1) |
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Baseline Aircraft Environmental Costs |
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294 | (1) |
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295 | (1) |
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Aircraft Designs for Reduced Noise |
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295 | (9) |
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295 | (1) |
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Baseline Aircraft Design and Noise Prediction |
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296 | (1) |
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Low Airframe Noise Design Methodology |
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297 | (1) |
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Low-Noise Aircraft Concept Brainstorming Process |
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297 | (2) |
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299 | (3) |
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Airframe Approach Noise Prediction |
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302 | (1) |
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303 | (1) |
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The Cranfield A-6 Greenliner Project |
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304 | (7) |
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Group Design Project Activities |
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304 | (1) |
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305 | (4) |
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Predicted Performance for the Greenliner |
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309 | (2) |
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311 | (2) |
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312 | (1) |
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Variational Approach to the Problem of the Minimum Induced Drag of Wings |
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313 | (30) |
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314 | (1) |
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314 | (2) |
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Problem of Minimum Induced Drag of a Straight Wing: An optimality condition |
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316 | (3) |
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Duality: A New Approach to the Design of Wings |
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319 | (6) |
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325 | (18) |
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325 | (2) |
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327 | (15) |
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342 | (1) |
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343 | (6) |
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343 | (4) |
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347 | (2) |
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348 | (1) |
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Problems of Minimal and Maximal Aerodynamic Resistance |
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349 | (18) |
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349 | (1) |
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350 | (5) |
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Translational Motion with Rotation: Two-Dimensional Case |
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355 | (12) |
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Definition of Rough Body and Mam Theorems |
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355 | (3) |
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Problems of Minimal and Maximal Resistance for a Slowly Rotating Body |
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358 | (2) |
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Mathematical Retroreflector |
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360 | (1) |
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361 | (4) |
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365 | (2) |
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Shock Optimization for Airfoil Design Problems |
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367 | (12) |
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Numerical Optimal Shape Design |
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367 | (3) |
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367 | (1) |
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368 | (1) |
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369 | (1) |
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Automatic Differentiation |
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370 | (2) |
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Principle of Automatic Differentiation |
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370 | (1) |
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371 | (1) |
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372 | (4) |
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Extended Calculus of Variation |
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372 | (1) |
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Sensitivity Analysis for Burgers' Equation |
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373 | (1) |
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Application to Optimal Control |
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373 | (1) |
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374 | (1) |
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374 | (2) |
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Small Disturbances and Automatic Differentiations |
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376 | (3) |
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377 | (2) |
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Differential Games Treated by a Gradient-Restoration Approach |
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379 | (18) |
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379 | (1) |
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Zero-Sum Differential Games |
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380 | (2) |
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Numerical Solution of Two-Sided Optimization Problems |
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382 | (3) |
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Transformation into Single-Objective Problem |
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382 | (2) |
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Sequential Gradient-Restoration Algorithm |
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384 | (1) |
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385 | (3) |
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Formulation of the Problem |
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385 | (1) |
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386 | (1) |
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387 | (1) |
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Orbital Pursuit-Evasion Game |
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388 | (7) |
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Formulation of the Problem |
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389 | (1) |
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390 | (2) |
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392 | (3) |
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395 | (2) |
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395 | (2) |
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Interval Methods for Optimal Control |
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397 | (22) |
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398 | (1) |
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Optimal and Robust Control of Dynamical Systems |
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399 | (4) |
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Optimal Control of Discrete and Continuous-Time Processes |
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400 | (1) |
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Specification of Robustness in the Time Domain |
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401 | (1) |
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Optimality Cateria for Systems with Uncertainties |
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402 | (1) |
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Interval Arithmetic Optimization Algorithm |
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403 | (2) |
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Parallelization of the Optimization Algorithm |
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405 | (1) |
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Combination with Classical Controller Design |
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406 | (1) |
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Validated Modeling and Simulation of Dynamical Systems with State-Dependent Switchings |
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407 | (3) |
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410 | (6) |
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Interval Algorithm for Structure Optimization |
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410 | (3) |
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Linear State Controller for Improvement of Robustness |
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413 | (2) |
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Interval Algorithm for Parameter Optimization |
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415 | (1) |
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Conclusions and Outlook on Future Work |
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416 | (3) |
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417 | (2) |
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Application of Optimisation Algorithms to Aircraft Aerodynamics |
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419 | (28) |
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419 | (5) |
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An Algorithm for the Search of Global Minima |
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424 | (4) |
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428 | (6) |
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Test Case 1 (Unconstrained): Ackley's Function |
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428 | (3) |
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Test Case 2 (Unconstrained): Rastrigin's Function |
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431 | (1) |
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Test Case 3 (Unconstrained): Rosenbrock's Function |
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431 | (1) |
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Test Case 4 (Unconstrained): Schwefel's Function |
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432 | (2) |
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The AEROSTATE Program: An Application to Aeronautics |
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434 | (11) |
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Minimum Induced Drag of a Wing |
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435 | (3) |
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Minimum Total Drag of a Wing |
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438 | (1) |
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439 | (2) |
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441 | (4) |
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445 | (2) |
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445 | (2) |
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Different levels of Optimisation in Aircraft Design |
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447 | (14) |
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448 | (1) |
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Industrial Process of Aircraft Design |
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449 | (3) |
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Different Levels of Aircraft Design vs. Development Phases |
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452 | (3) |
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Tools Used in Different Phases |
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455 | (4) |
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459 | (2) |
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459 | (2) |
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Numerical and Analytical Methods for Global Optimization |
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461 | (16) |
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461 | (2) |
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463 | (6) |
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469 | (5) |
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474 | (3) |
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474 | (3) |
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The Aeroservoelasticity Qualification Process in Alenia |
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477 | (14) |
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477 | (1) |
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478 | (1) |
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479 | (1) |
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Aeroelastic Tradition in Alenia |
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480 | (1) |
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Aeroservoelastic Certification Process |
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481 | (10) |
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482 | (2) |
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484 | (2) |
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486 | (1) |
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486 | (1) |
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Research and Future Developments |
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486 | (5) |
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Further Steps Towards Quantitative Conceptual Aircraft Design |
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491 | (18) |
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491 | (5) |
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The Systems Engineering Approach |
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496 | (1) |
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Requirements on Computational Systems |
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496 | (1) |
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The Design and Engineering Engine Concept |
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497 | (8) |
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Describing Design Options |
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497 | (4) |
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501 | (2) |
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The Multi-model Generator |
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503 | (1) |
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The Life-Cycle Analysis with Expert Tools |
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504 | (1) |
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504 | (1) |
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The Agent-Based Framework |
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504 | (1) |
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505 | (2) |
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507 | (2) |
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508 | (1) |
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Some Plebeian Variational Problems |
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509 | |
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509 | |
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Mechanical Plebeian Problems |
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510 | |
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513 | |
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515 | |
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518 | |
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518 | |