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Copyright of Journal of Engineering for Thermal Energy & Power / Reneng Dongli Gongcheng is the property of Journal of Engineering for Thermal Energy & Power and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)

Copyright of Journal of Engineering for Thermal Energy & Power / Reneng Dongli Gongcheng is the property of Journal of Engineering for Thermal Energy & Power and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)

Inflow temperature distortion is an influential factor to determine the stable work margin of aero-engine. In current paper, an overview of temperature distortion introduction mechanism is first reviewed. Fundamental study concerning temperature distortion introduction mechanism is presented. Summarization is given about influence of temperature distortion on propulsion component characteris tics and the aero-engine overall performance. Then comparative study is made based on currently applied temperature distortion simulation devices as well as their operation mechanisms. Progress made in both fundamental and applied research with the aid of temperature distortion simulation devices is introduced.In addition, inflow temperature distortion assessment methodology as well as corresponding standard is introduced with highlight on key techniques concerning temperature distortion test. Finally, techniques to mitigate temperature distortion on aero-engine are summarized and trade study is made upon those techniques. Aero-engine temperature distortion research will provide guidance for engine temperature resistance design and test. [ABSTRACT FROM AUTHOR]