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CASTING OPTIMIZED TO IMPROVE SUCTION SIDE COOLING SHAPED HOLE PERFORMANCE
CASTING OPTIMIZED TO IMPROVE SUCTION SIDE COOLING SHAPED HOLE PERFORMANCE
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机译:优化铸件以提高吸风侧冷却的异型孔性能
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摘要
A gas turbine engine component includes a pressure side, a suction side, a leading edge, a trailing edge, an outer surface and an inner surface. The inner surface is positioned within the outer surface and defines a core. The inner surface has a first protrusion.
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