Control of an oblique shock/boundary-layer interaction with aeroelastic mesoflaps

Keyphrases

• Flap 100%
• Shock Wave Boundary Layer Interaction 100%
• Aeroelasticity 100%
• Oblique Shock 100%
• Shock 66%
• Bleeding 66%
• Boundary Layer Thickness 66%
• Performance Improvement 33%
• Flow Visualization 33%
• Deflection 33%
• Mid-plane 33%
• Solid Wall 33%
• Pressure Profile 33%
• Flow Condition 33%
• Control Strategy 33%
• Stagnation Pressure 33%
• Shock Interaction 33%
• Recirculating 33%
• Velocity Measurement 33%
• Recirculation 33%
• Pressure Loading 33%
• Gas Dynamics 33%
• Shadowgraphy 33%
• Passive Cavity 33%
• Mean Velocity 33%
• Span-wise 33%
• Supersonic Wind Tunnel 33%
• Transpiration 33%
• Small Flap 33%
• Flow Injection 33%
• Three-dimensional Effect 33%
• Improved Recovery 33%
• Fluctuating Velocity 33%
• Unit Reynolds number 33%
• Enclosed Cavity 33%
• Shock Impingement 33%
• Reduced Boundary 33%
• Surface Pressure Measurement 33%

Engineering

• Boundary Layer 100%
• Layer Interaction 100%
• Flaps 100%
• Oblique Shock 100%
• Boundary Layer Thickness 50%
• Flow Visualization 25%
• Applicability 25%
• Reynolds' Number 25%
• Flow Condition 25%
• Performance Improvement 25%
• Control Strategy 25%
• Shock Interaction 25%
• Stagnation Pressure 25%
• Solid Wall 25%
• Pressure Profile 25%
• Shadowgraph 25%
• Fluctuating Velocity 25%
• Shock Impingement 25%
• Tunnel 25%