Bypass transition in boundary layers including curvature and favorable pressure gradient effects

Keyphrases

• Boundary Layer 100%
• Skin Friction 100%
• Production Rate 100%
• Free-stream Turbulence 100%
• Bypass Transition 100%
• Pressure Gradient Effect 100%
• Convex Curvature 100%
• Favorable Pressure Gradient 100%
• Transition Region 66%
• Turbulence Level 66%
• Reynolds number 66%
• Inconsistency 66%
• Flat Wall 66%
• Stanton number 66%
• Intermittency 66%
• Two Dimensional 33%
• Streamwise 33%
• Correlation Value 33%
• Fully Turbulent 33%
• Reynolds Analogy 33%
• Integral Solution 33%
• Turbulent Region 33%
• Görtler Vortices 33%
• Onset Location 33%
• Transition Length 33%
• Momentum Thickness 33%
• Wall Skin Friction 33%
• Turbulent Spot 33%
• Acceleration Effect 33%
• Wall Curvature 33%
• Laminar Region 33%
• Scale Measurement 33%
• Local Boundary 33%
• Freestream Disturbances 33%
• Enhanced Turbulence 33%

Engineering

• Boundary Layer 100%
• Pressure Gradient 100%
• Skin-Friction Coefficient 66%
• Reynolds' Number 66%
• Stanton Number 66%
• Streamwise 33%
• Two Dimensional 33%
• Length Scale 33%
• Momentum Thickness 33%
• Reynolds Analogy 33%
• Scale Measurement 33%
• Laminar Region 33%
• Skin Friction 33%