Pages that link to "Item:Q3720139"
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The following pages link to Inverse method with geometric constraints for transonic aerofoil design (Q3720139):
Displaying 19 items.
- Wing design for supersonic transports using integral equation method (Q597639) (← links)
- Shock-free transonic airfoils with a given pressure distribution (Q1083310) (← links)
- An inverse method with regularity condition for transonic airfoil design (Q1194833) (← links)
- Compressible flow airfoil design using natural coordinates (Q1912179) (← links)
- Optimum transonic airfoils based on the Euler equations (Q1973765) (← links)
- An inverse design method for non-uniform flow inlet with a given shock wave (Q2316296) (← links)
- Coupled problem of the inverse design and constraint optimization (Q2451291) (← links)
- An inverse approach for airfoil design (Q2920575) (← links)
- A non-iterative technique for design of aerofoils in incompressible potential flow (Q3197523) (← links)
- Role of constraints in inverse design for transonic airfoils (Q3216330) (← links)
- A quasi three-dimensional inverse design method using source and vortex integral equations (Q3720122) (← links)
- The design of transonic aerofoils by a well‐posed inverse method (Q3720140) (← links)
- Application of elliptic continuation method for transonic aerofoil design and experimental verification (Q3720144) (← links)
- An engineering approach to the inverse transonic wing design problem (Q3720150) (← links)
- Subsonic airfoils with a given pressure distribution (Q3770190) (← links)
- An exact inverse method for subsonic flows (Q3813494) (← links)
- Multipoint inverse airfoil design method based on conformal mapping (Q3992308) (← links)
- Aspects of the transpiration model for aerofoil design (Q4289545) (← links)
- An inverse design method for engine nacelles and wings (Q5491304) (← links)
