Pages that link to "Item:Q1648458"
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The following pages link to The effects of Mach number on the flow separation control of airfoil with a small plate near the leading edge (Q1648458):
Displaying 4 items.
- The influence of acceleration and deceleration on shock wave movement on and around aerofoils in transonic flight (Q1932276) (← links)
- (Q5005367) (← links)
- A comprehensive comparison of passive flow controls on the wind turbine blade lift and drag performances: a CFD approach (Q6621923) (← links)
- A review on 2-D supersonic aerofoil shape optimization (Q6656387) (← links)