Pages that link to "Item:Q3720121"
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The following pages link to The role of a mixed design and analysis method in a turbomachinery blade design system (Q3720121):
Displaying 5 items.
- Finite element analysis and redesign of a compressor hub spinner (Q1389692) (← links)
- Computational methods for aerodynamic shape design (Q1842788) (← links)
- Shock-free transonic rotor design (Q3730244) (← links)
- A design method for two-dimensional cascades of turbomachinery blades (Q3776872) (← links)
- A design method for turbomachinery blading in three‐dimensional flow (Q4206494) (← links)