Numerical Investigation of Unsteady Boundary Layer Transition on a Dynamically Pitching Rotor

Keyphrases

• Numerical Investigation 100%
• Rotor 100%
• Boundary Layer Transition 100%
• Unsteady Boundary Layer 100%
• Transition Prediction 66%
• Transition Modeling 66%
• Laminar-turbulent Transition 66%
• Computational Methods 33%
• Performance Prediction 33%
• Mach number 33%
• Wind Tunnel 33%
• Computational Fluid Dynamics Modeling 33%
• Hovering 33%
• Turbulence Intensity 33%
• Free-stream Turbulence 33%
• Computational Grid 33%
• Rotor Test 33%
• Aerospace 33%
• Rotor Performance 33%
• Grid Generation 33%
• Bladed Rotor 33%
• Hybrid RANS-LES 33%
• Rotor Flow Field 33%

Engineering

• Rotors 100%
• Boundary Layer Transition 100%
• Laminar-Turbulent Transition 40%
• Test Facility 20%
• Experimental Measurement 20%
• Computational Fluid Dynamics 20%
• Mach Number 20%
• NASA 20%
• Turbulence Intensity 20%
• Prediction Performance 20%
• Rotor Performance 20%
• Grid Generation 20%
• Flow Distribution 20%
• Tunnel 20%

Physics

• Boundary Layer Transition 100%
• Laminar-Turbulent Transition 66%
• Flow Distribution 33%
• Computational Method 33%
• Wind Tunnels 33%
• Mach Number 33%
• Computational Fluid Dynamics 33%