Experimental study on thermal protection system by opposing jet in supersonic flow

Physics

• Aerodynamic Heating 100%
• Supersonic Flow 66%
• Diameters 33%
• Ratios 33%
• Region 33%
• High Pressure 33%
• Mach Number 33%
• Protection System 33%
• Blunt Bodies 33%

Engineering

• Reduction 100%
• Pressure Ratio 66%
• Surface Model 33%
• Freestream 33%
• High Pressure 33%
• Heat Flux 33%
• Blunt Body 33%
• Thermal Protection 33%