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Impact of Different Film-Cooling Modes at Leading Edge on the Aerodynamic and Heat Transfer Performance of Heavy Duty Gas Turbine

✍ Scribed by Lu, Shaopeng ;Liu, Xun ;Wang, Songtao ;Zhou, Xun ;Feng, Guotai ;Wang, Zhongqi


Book ID
115476054
Publisher
IEEE
Year
2012
Weight
425 KB
Series
undefined series for scimag
Category
Article

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Three-dimensional flow and heat transfer
✍ D. Lakehal; G.S. Theodoridis; W. Rodi 📂 Article 📅 2001 🏛 Elsevier Science 🌐 English ⚖ 1007 KB

Film cooling of a symmetrical turbine-blade model by lateral and non-lateral injection from one row of holes placed on each side near the leading edge is calculated with a 3D ®nite-volume method on multi-block grids. For various blowing rates, the ¯ow and temperature ®elds are predicted, and in part