Numerical investigation of oblique-shock/boundary-layer interactions in supersonic flows

Keyphrases

• Numerical Investigation 100%
• Direct numerical Simulation 100%
• Separation Bubble 100%
• Shock Waves 100%
• Supersonic Flow 100%
• Shock Wave Boundary Layer Interaction 100%
• Oblique Shock 100%
• Arizona 50%
• Shock 50%
• Reynolds number 50%
• Incidence Angle 50%
• Mach number 50%
• Free Stream 50%
• Transition Process 50%
• Laminar Separation Bubble 50%
• Laminar Boundary Layer 50%
• Flat Plate 50%
• Low Amplitude 50%
• Laminar-turbulent Transition 50%
• Steady Flow 50%
• Linear Stability 50%
• Flow Parameters 50%
• Stability Behavior 50%
• Approach Flow 50%
• Linearized Navier-Stokes 50%
• Flow Field Calculation 50%

Engineering

• Boundary Layer 100%
• Direct Numerical Simulation 100%
• Separation Bubble 100%
• Supersonic Flow 100%
• Layer Interaction 100%
• Shockwave 100%
• Oblique Shock 100%
• Flow Field 50%
• Reynolds' Number 50%
• Mach Number 50%
• Linearized Stability 50%
• Laminar Boundary Layer 50%
• Laminar Separation Bubble 50%
• Flat Plate 50%
• Steady Flow 50%
• Incidence Angle 50%
• Conducted Experiment 50%
• Flow Parameters 50%
• Laminar-Turbulent Transition 50%