..

天体物理学与航空航天技术

Part Design of an Aero Engine's High-Pressure Turbine

Abstract

Tobias Guggemos

The essential exploration of this paper is introduced as follows: the actual system of changes in turbine, first and foremost, tip freedom was concentrated on in light of the primary standard as per the underlying qualities, working rule, and establishment climate of turbine parts. Moreover, the primary and optional elements influencing changes in the tip leeway were filtered out as per the significance of the effect on changes.

免责声明: 此摘要通过人工智能工具翻译,尚未经过审核或验证

分享此文章

索引于

相关链接

arrow_upward arrow_upward