Pages that link to "Item:Q3776872"
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The following pages link to A design method for two-dimensional cascades of turbomachinery blades (Q3776872):
Displaying 9 items.
- Influence of exit-to-throat width ratio on performance of high pressure convergent-divergent rotor in a vaneless counter-rotating turbine (Q546570) (← links)
- An inverse calculation technique for quasi-three-dimensional turbomachinery cascades (Q687018) (← links)
- A software tool for parametric design of turbomachinery blades (Q948810) (← links)
- Turbine blade design by lofted B-spline surfaces (Q1576460) (← links)
- A method of calculating the flow around and aerodynamic design of the profiles of turbomachinery blade grids (Q1803127) (← links)
- Two-dimensional RANS simulations of the flow through a compressor cascade with jet flaps (Q2853538) (← links)
- Thin turbomachinery blade design using a finite-volume method (Q3219971) (← links)
- The role of a mixed design and analysis method in a turbomachinery blade design system (Q3720121) (← links)
- A design method for turbomachinery blading in three‐dimensional flow (Q4206494) (← links)