Pages that link to "Item:Q1622191"
From MaRDI portal
The following pages link to Euler-based throughflow method for inverse design and optimisation of turbomachinery blades (Q1622191):
Displaying 8 items.
- 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)
- A fast iterative inverse method for turbomachinery blade design (Q1939928) (← links)
- A penalty formulation for the throughflow modeling of turbomachinery (Q2361816) (← links)
- Partially reduced SQP methods for optimal turbine and compressor blade design (Q2704837) (← links)
- An inverse blade design method for subsonic and transonic viscous flow in compressors and turbines (Q3588278) (← links)
- Three-dimensional viscous inverse method for axial blade design (Q3647591) (← links)
- Inverse design of multiholed internally cooled turbine blades (Q3722091) (← links)