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...
المؤلفون الرئيسيون: | Vieira, J, Coull, J, Ireland, P, Romero, E |
---|---|
التنسيق: | Journal article |
اللغة: | English |
منشور في: |
American Society of Mechanical Engineers
2021
|
مواد مشابهة
-
An experimental investigation of adiabatic film cooling effectiveness and heat transfer coefficient on a transonic squealer tip
حسب: Saul, A, وآخرون
منشور في: (2019) -
Inclined slot cooling of the pressure side rims of squealer tips
حسب: Vieira, JAC, وآخرون
منشور في: (2022) -
Three-dimensional optimization of squealer-tip for a transonic axial-flow compressor rotor blade
حسب: Mojtaba Heidarian Shahri, وآخرون
منشور في: (2024-01-01) -
Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
حسب: Yufan Wang, وآخرون
منشور في: (2022-01-01) -
Transonic Turbine Blade Tip Aerothermal Performance With Different Tip Gaps-Part I: Tip Heat Transfer
حسب: Zhang, Q, وآخرون
منشور في: (2011)