Pages that link to "Item:Q3588278"
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The following pages link to An inverse blade design method for subsonic and transonic viscous flow in compressors and turbines (Q3588278):
Displaying 12 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)
- Euler-based throughflow method for inverse design and optimisation of turbomachinery blades (Q1622191) (← links)
- A fast iterative inverse method for turbomachinery blade design (Q1939928) (← links)
- An inverse design method for cascades for low-Reynolds number flow (Q1954342) (← links)
- A new Navier-Stokes inverse method based on mass-averaged tangential velocity for blade design (Q3624548) (← links)
- An inverse design method for viscous flow in turbomachinery blading using a wall virtual movement (Q3630071) (← links)
- Three-dimensional viscous inverse method for axial blade design (Q3647591) (← links)
- Inverse design of supercritical nozzles and cascades (Q3720145) (← links)
- On the use of inverse modes of calculation in two-dimensional cascades and ducts (Q3720152) (← links)
- Inverse design of multiholed internally cooled turbine blades (Q3722091) (← links)
- A design method for turbomachinery blading in three‐dimensional flow (Q4206494) (← links)