Aerothermal effect of cavity welding beads on a transonic squealer tip
<p>High-pressure turbine blade tips are critical for gas turbine performance and are sensitive to small geometric variations. For this reason, it is increasingly important for experiments and simulations to consider real geometry features. One commonly absent detail is the presence of welding...
Hoofdauteurs: | Vieira, J, Coull, J, Ireland, P, Romero, E |
---|---|
Formaat: | Journal article |
Taal: | English |
Gepubliceerd in: |
American Society of Mechanical Engineers
2021
|
Gelijkaardige items
-
An experimental investigation of adiabatic film cooling effectiveness and heat transfer coefficient on a transonic squealer tip
door: Saul, A, et al.
Gepubliceerd in: (2019) -
Inclined slot cooling of the pressure side rims of squealer tips
door: Vieira, JAC, et al.
Gepubliceerd in: (2022) -
Three-dimensional optimization of squealer-tip for a transonic axial-flow compressor rotor blade
door: Mojtaba Heidarian Shahri, et al.
Gepubliceerd in: (2024-01-01) -
Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
door: Yufan Wang, et al.
Gepubliceerd in: (2022-01-01) -
Transonic Turbine Blade Tip Aerothermal Performance With Different Tip Gaps-Part I: Tip Heat Transfer
door: Zhang, Q, et al.
Gepubliceerd in: (2011)