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...
主要な著者: | Vieira, J, Coull, J, Ireland, P, Romero, E |
---|---|
フォーマット: | Journal article |
言語: | English |
出版事項: |
American Society of Mechanical Engineers
2021
|
類似資料
-
An experimental investigation of adiabatic film cooling effectiveness and heat transfer coefficient on a transonic squealer tip
著者:: Saul, A, 等
出版事項: (2019) -
Inclined slot cooling of the pressure side rims of squealer tips
著者:: Vieira, JAC, 等
出版事項: (2022) -
Three-dimensional optimization of squealer-tip for a transonic axial-flow compressor rotor blade
著者:: Mojtaba Heidarian Shahri, 等
出版事項: (2024-01-01) -
Numerical Study on Vortex Structures and Loss Characteristics in a Transonic Turbine with Various Squealer Tips
著者:: Yufan Wang, 等
出版事項: (2022-01-01) -
Transonic Turbine Blade Tip Aerothermal Performance With Different Tip Gaps-Part I: Tip Heat Transfer
著者:: Zhang, Q, 等
出版事項: (2011)