Transition delay in hypervelocity boundary layers by means of CO ₂/acoustic instability interactions

Keyphrases

• Hypervelocity 100%
• Boundary Layer 100%
• CO 2 100%
• Computational Data 100%
• Acoustic Instability 100%
• Transition Delay 100%
• University of Minnesota 50%
• Vehicle Engineering 50%
• Hypersonic Vehicle 50%
• Free Stream 50%
• Vibrational Modes 50%
• Thermocouple 50%
• California Institute of Technology 50%
• Heat Transfer Measurement 50%
• Numerical Data 50%
• Shadowgraphy 50%
• Transition Location 50%
• Transitional Reynolds number 50%
• C4F7N/CO2 50%
• Slender Body 50%
• CO2 Mole Fraction 50%
• Layer of Interest 50%
• Injection Scheme 50%
• T5 Reflected Shock Tunnel 50%
• Injection Timing 50%
• Sharp Cone 50%
• Hypervelocity Flow 50%

Engineering

• Boundary Layer 100%
• Vehicle Design 50%
• Reynolds' Number 50%
• Mole Fraction 50%
• Axisymmetric 50%
• Thermocouple 50%
• Experimental Model 50%
• Shadowgraph 50%
• Reflected Shock 50%
• Numerical Data 50%
• Slender Body 50%
• Hypersonic Vehicle 50%