基于变精度模型的变外形飞行器弹道优化

Engineering

• Aerodynamics 100%
• Angle-of-Attack 100%
• Optimal Trajectory 100%
• Control Parameter 100%
• Mach Number 50%
• Kriging Model 50%
• Computational Fluid Dynamics 50%
• Flight Condition 50%
• Fixed Wings 50%
• Sweep Angle 50%
• Aerodynamic Performance 50%
• Engine Control 50%
• Model Fidelity 50%
• Flow Solution 50%