Experimental and computational study on reduction of aerodynamic heating load by film cooling in hypersonic flows

Physics

• Heat 100%
• Protection 100%
• Film Cooling 100%
• Boundary Layer 66%
• Blunt Bodies 66%
• Hypersonic Flow 66%
• Model 33%
• Gases 33%
• Wind Tunnels 33%
• Turbulence Model 33%
• Navier-Stokes Equation 33%
• Numerical Analysis 33%
• Coolant 33%
• Aerodynamic Heating 33%
• Low Reynolds Number 33%
• Compressibility 33%

Engineering

• Experiments 100%
• Surfaces 66%
• Blunt Body 66%
• Models 33%
• Good Agreement 33%
• Reduction 33%
• Characteristics 33%
• Compressibility 33%
• Axisymmetric 33%
• Numerical Analysis 33%
• Thermal Loads 33%
• Finite Difference Method 33%
• Heat Flux 33%
• Low Reynolds Number 33%
• Navier-Stokes Equation 33%
• Significant Decrease 33%
• Cooling Effect 33%
• Blowdown 33%