多功能平板热管的传热性能实验研究

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中图分类号：V216.4 文献标志码：A 文章编号：1671-5276（2025）05-0017-04

DONG Ao，GUO Ce，SHEN Jingyu，ZHENG Wei，ZHANG Zhen （Nanjing University of Aeronautics and Astronautics，Nanjing 2lool6，China） Abstract：To meet thermal protection and carrying requirementsof hypersonic vehicle during flight，this paper proposes a novel structure integrated thermal management and carying.The analysis on thermal performance of the structure by experiment verifies thatthe flat heat pipe structure hasa superior isotherm.Inaddition，theinfluenceof parameters such as the filling rate，gravity and working fluid on thermal performance is further analyzed through experiment. Keywords：vehicle;bionic sandwich;flat heat pipe;thermal performance;integrated structure

0 引言

高超声速飞行器往往指以马赫数5以上的速度远程巡航飞行的飞行器[1]。（剩余5568字）