Experimental investigation of the performance of a loop heat pipe-based cooling system under ultra-high dypass ratio turbojet engine conditions

The subject of this article is the heat transfer processes in a loop heat pipe (LHP) to solve the problem of maintaining the temperature regime of the valves of the air-bleeding system of an aircraft engine. The goal was to experimentally substantiate the operability and efficiency of a cooling syst...

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Bibliographic Details
Main Authors: Pavlo Gakal, Igor Rybalchenko, Oleksii Tretyak, Viacheslav Nazarenko
Format: Article
Language:English
Published: National Aerospace University «Kharkiv Aviation Institute» 2025-01-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/2739