NUMERICAL THERMAL ANALYSIS OF RE-ENTRY APOLLO MODEL AS-202 AT HIGH ANGLE OF ATTACK

Engineering

• Angle-of-Attack 100%
• Equivalent Stress 66%
• Attack Angle 66%
• Computational Fluid Dynamics 33%
• Pressure Distribution 33%
• Temperature Distribution 33%
• Finite Element Analysis 33%
• Physical Phenomena 33%
• Nonlinear Partial Differential Equation 33%
• Thermal Load 33%
• Thermal Stress 33%
• Free Flow 33%

Material Science

• Finite Element Method 100%
• Computational Fluid Dynamics 100%
• Thermal Stress 100%
• Thermal Analysis 100%