Pages that link to "Item:Q1939928"
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The following pages link to A fast iterative inverse method for turbomachinery blade design (Q1939928):
Displaying 11 items.
- A software tool for parametric design of turbomachinery blades (Q948810) (← links)
- Euler-based throughflow method for inverse design and optimisation of turbomachinery blades (Q1622191) (← links)
- An adjoint approach to optimal design of turbine blades (Q1772788) (← links)
- A method of calculating the flow around and aerodynamic design of the profiles of turbomachinery blade grids (Q1803127) (← links)
- Partially reduced SQP methods for optimal turbine and compressor blade design (Q2704837) (← links)
- Thin turbomachinery blade design using a finite-volume method (Q3219971) (← links)
- An inverse blade design method for subsonic and transonic viscous flow in compressors and turbines (Q3588278) (← links)
- A new Navier-Stokes inverse method based on mass-averaged tangential velocity for blade design (Q3624548) (← links)
- Three-dimensional viscous inverse method for axial blade design (Q3647591) (← links)
- The role of a mixed design and analysis method in a turbomachinery blade design system (Q3720121) (← links)
- Inverse design of multiholed internally cooled turbine blades (Q3722091) (← links)