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Method and structure for cooling airfoil surfaces using asymmetric angle film holes
Method and structure for cooling airfoil surfaces using asymmetric angle film holes
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机译:使用不对称角膜孔冷却翼型件表面的方法和结构
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摘要
A film cooled turbine structure is configured with one or more asymmetrical angular film cooling holes to improve film cooling for a variety of areas, particularly in areas and applications where the surface fluid flow line curvature is significant.
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