Pages that link to "Item:Q1649639"
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The following pages link to Comparative study of boundary layer control around an ordinary airfoil and a high lift airfoil with secondary blowing (Q1649639):
Displaying 3 items.
- The effects of Mach number on the flow separation control of airfoil with a small plate near the leading edge (Q1648458) (← links)
- Delay or control of flow separation for enhanced aerodynamic performance using an effective morphed surface (Q2141495) (← links)
- Investigation of the possibility of boundary layer control at the parts of aircraft (Q2755190) (← links)