3D CFD Research of Labyrinth Seal Cavities of Aircraft Turbine Engine

M. Čížek
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引用次数: 3

Abstract

This article describes and graphical clarify the air flow through the labyrinth seals of aircraft turbine engine. Evaluates the air flow data from the calculation and define the high temperature gradient in labyrinth seal.
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航空涡轮发动机迷宫式密封腔的三维CFD研究
本文对航空涡轮发动机迷宫式密封件的气流进行了描述和图解说明。对计算得到的气流数据进行评估,确定了迷宫密封的高温梯度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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