Pages that link to "Item:Q1083310"
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The following pages link to Shock-free transonic airfoils with a given pressure distribution (Q1083310):
Displaying 10 items.
- Wing design for supersonic transports using integral equation method (Q597639) (← links)
- Example of solving transonic equations for a shock-free flow past a symmetric profile (Q1060918) (← links)
- An inverse design method for non-uniform flow inlet with a given shock wave (Q2316296) (← links)
- Inverse design of supercritical nozzles and cascades (Q3720145) (← links)
- Shock-free redesign using finite elements (Q3720147) (← links)
- (Q3727615) (← links)
- Shock-free transonic rotor design (Q3730244) (← links)
- The design of shock-free supercritical airfoils including viscous effects (Q3741284) (← links)
- Subsonic airfoils with a given pressure distribution (Q3770190) (← links)
- Transonic equivalence rule involving lift and shocks (Q4373155) (← links)