Pages that link to "Item:Q1317728"
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The following pages link to Maximization of the critical Mach number for lifting airfoils (Q1317728):
Displaying 4 items.
- Maximization of the lift/drag ratio of airfoils with a turbulent boundary layer (Q1289508) (← links)
- On the design of lifting airfoils with high critical Mach number using full potential theory (Q1371498) (← links)
- Bilateral estimates of the critical Mach number for some classes of carrying wing profiles (Q2725327) (← links)
- Lift maximization in the flow around a contour over a screen (Q5311023) (← links)