Comparative study of various approaches for modeling transitional hypersonic rarefied gas flows over blunt bodies

Engineering

• Flow Regime 100%
• Rarefied Gas Flows 100%
• Blunt Body 100%
• Applicability 50%
• Direct Simulation 50%
• Axisymmetric 50%
• Boltzmann Equation 50%
• Kinetic Equation 50%
• Knudsen Number 50%
• Continuum Approach 50%
• Space Vehicle 50%
• Hypersonic Flows 50%
• Numerical Solution 50%

Physics

• Rarefied Gas Flows 100%
• Hypersonics 100%
• Blunt Body 100%
• Numerical Solution 50%
• Space Vehicle 50%
• Hypersonic Flow 50%
• Free Flow 50%
• Monte Carlo Method 50%
• Knudsen Flow 50%
• Kinetic Equation 50%
• Reentry 50%