Pages that link to "Item:Q1261811"
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The following pages link to On the construction and calculation of optimal nonlifting critical airfoils (Q1261811):
Displaying 15 items.
- Thin airfoils of minimum wave drag with given chord, longitudinal section area, and lift (Q1304564) (← links)
- Maximization of the critical Mach number for lifting airfoils (Q1317728) (← links)
- On an extremal problem of airfoil theory (Q1589373) (← links)
- Construction of airfoils and engine nacelles that are supercritical in a transonic perfect-gas flow (Q1608292) (← links)
- Hodograph design of lifting airfoils with high critical Mach numbers (Q1892195) (← links)
- Plane and axisymmetric bodies in a flow with the greatest ``critical'' Mach number (Q2172686) (← links)
- On the curvature of boundary streamlines of an ideal gas at separation and reattachment points (Q2686669) (← links)
- Bilateral estimates of the critical Mach number for some classes of carrying wing profiles (Q2725327) (← links)
- (Q3328061) (← links)
- The Sears problem for a lifting airfoil revisited - new results (Q3343611) (← links)
- (Q3363691) (← links)
- Calculating the lift on a finite stack of cylindrical aerofoils (Q3503318) (← links)
- (Q4518531) (← links)
- Transonic flows of single-phase supercritical fluids over thin airfoils (Q5858621) (← links)
- Lift airfoils close to the airfoils in a flow with the maximum ``critical'' Mach numbers (Q6169706) (← links)