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...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
National Aerospace University «Kharkiv Aviation Institute»
2025-01-01
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Series: | Авіаційно-космічна техніка та технологія |
Subjects: | |
Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/2739 |