Study on Dynamic Characteristics of Mars Entry Module in Transonic and Supersonic Speeds

Engineering

• Supersonic Speed 100%
• Angle-of-Attack 66%
• Computational Cost 33%
• Computer Simulation 33%
• Mach Number 33%
• Rigid Structure 33%
• Degree of Freedom 33%
• Dynamic Stability 33%
• Simulation Method 33%
• Computational Fluid Dynamics 33%
• Large Eddy Simulation 33%
• Engineering Calculation 33%
• Unsteady Flow 33%
• Reynolds-Averaged Navier-Stokes 33%
• Direct Numerical Simulation 33%
• Dynamic Instability 33%
• Detached Eddy Simulation 33%
• Body Shape 33%