Maolin Ke , Jinxing Zheng , Haiyang Liu , Yifan Du , Bin Zhao , Pinghui Zhao , Meiqi Wu , Yudong Lu
{"title":"磁等离子体动力推力器高热负荷曲面的湍流拓扑优化热结构设计","authors":"Maolin Ke , Jinxing Zheng , Haiyang Liu , Yifan Du , Bin Zhao , Pinghui Zhao , Meiqi Wu , Yudong Lu","doi":"10.1016/j.ijthermalsci.2025.110037","DOIUrl":null,"url":null,"abstract":"<div><div>In the past decade, with the rise of space propulsion, MagnetoPlasmaDynamic Thrusters(MPDT) have been favored due to their stronger performance. However, a considerable part of the electrical energy is dissipated in the form of heat at the anode, resulting in excessive temperature, which reduces the performance of the propeller. In order to alleviate this situation, liquid cooling system is necessary.</div><div>This study designed a new cooling channel using the k-ε turbulence topology optimization method for the high heat load curved surface of the MPD thruster,and demonstrated the improvement of thermal hydraulic performance through numerical simulation and experiments. We have studied the influence of weight factors and different objective functions on the results of topology optimization design, and believe that the multi-objective optimization combination of dissipation and temperature averaging is more appropriate. When the inlet velocity is 0.7 m/s, topology optimization design reduces the pressure drop of the flow channel by 11.3 %–16.2 %, reduces the thermal resistance by 0.0037–0.0054 W/K, and increases the Nusselt number by 35.5 %–84.1 % compared to traditional design. This study provides guidance for channel design under high heat load surfaces at higher Reynolds numbers using turbulent topology optimization methods.</div><div>Considering the machining difficulty and the thermo-hydraulic properties, the To<sub>A,6</sub> model were fabricated and machined and tested experimentally, and the experimental results were in agreement with the numerical simulations.</div></div>","PeriodicalId":341,"journal":{"name":"International Journal of Thermal Sciences","volume":"217 ","pages":"Article 110037"},"PeriodicalIF":4.9000,"publicationDate":"2025-06-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Turbulent topology optimized thermal structure design for curved surfaces with high heat loads in MagnetoPlasmaDynamic Thrusters\",\"authors\":\"Maolin Ke , Jinxing Zheng , Haiyang Liu , Yifan Du , Bin Zhao , Pinghui Zhao , Meiqi Wu , Yudong Lu\",\"doi\":\"10.1016/j.ijthermalsci.2025.110037\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>In the past decade, with the rise of space propulsion, MagnetoPlasmaDynamic Thrusters(MPDT) have been favored due to their stronger performance. However, a considerable part of the electrical energy is dissipated in the form of heat at the anode, resulting in excessive temperature, which reduces the performance of the propeller. In order to alleviate this situation, liquid cooling system is necessary.</div><div>This study designed a new cooling channel using the k-ε turbulence topology optimization method for the high heat load curved surface of the MPD thruster,and demonstrated the improvement of thermal hydraulic performance through numerical simulation and experiments. We have studied the influence of weight factors and different objective functions on the results of topology optimization design, and believe that the multi-objective optimization combination of dissipation and temperature averaging is more appropriate. When the inlet velocity is 0.7 m/s, topology optimization design reduces the pressure drop of the flow channel by 11.3 %–16.2 %, reduces the thermal resistance by 0.0037–0.0054 W/K, and increases the Nusselt number by 35.5 %–84.1 % compared to traditional design. This study provides guidance for channel design under high heat load surfaces at higher Reynolds numbers using turbulent topology optimization methods.</div><div>Considering the machining difficulty and the thermo-hydraulic properties, the To<sub>A,6</sub> model were fabricated and machined and tested experimentally, and the experimental results were in agreement with the numerical simulations.</div></div>\",\"PeriodicalId\":341,\"journal\":{\"name\":\"International Journal of Thermal Sciences\",\"volume\":\"217 \",\"pages\":\"Article 110037\"},\"PeriodicalIF\":4.9000,\"publicationDate\":\"2025-06-16\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Thermal Sciences\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1290072925003606\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, MECHANICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Thermal Sciences","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1290072925003606","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
Turbulent topology optimized thermal structure design for curved surfaces with high heat loads in MagnetoPlasmaDynamic Thrusters
In the past decade, with the rise of space propulsion, MagnetoPlasmaDynamic Thrusters(MPDT) have been favored due to their stronger performance. However, a considerable part of the electrical energy is dissipated in the form of heat at the anode, resulting in excessive temperature, which reduces the performance of the propeller. In order to alleviate this situation, liquid cooling system is necessary.
This study designed a new cooling channel using the k-ε turbulence topology optimization method for the high heat load curved surface of the MPD thruster,and demonstrated the improvement of thermal hydraulic performance through numerical simulation and experiments. We have studied the influence of weight factors and different objective functions on the results of topology optimization design, and believe that the multi-objective optimization combination of dissipation and temperature averaging is more appropriate. When the inlet velocity is 0.7 m/s, topology optimization design reduces the pressure drop of the flow channel by 11.3 %–16.2 %, reduces the thermal resistance by 0.0037–0.0054 W/K, and increases the Nusselt number by 35.5 %–84.1 % compared to traditional design. This study provides guidance for channel design under high heat load surfaces at higher Reynolds numbers using turbulent topology optimization methods.
Considering the machining difficulty and the thermo-hydraulic properties, the ToA,6 model were fabricated and machined and tested experimentally, and the experimental results were in agreement with the numerical simulations.
期刊介绍:
The International Journal of Thermal Sciences is a journal devoted to the publication of fundamental studies on the physics of transfer processes in general, with an emphasis on thermal aspects and also applied research on various processes, energy systems and the environment. Articles are published in English and French, and are subject to peer review.
The fundamental subjects considered within the scope of the journal are:
* Heat and relevant mass transfer at all scales (nano, micro and macro) and in all types of material (heterogeneous, composites, biological,...) and fluid flow
* Forced, natural or mixed convection in reactive or non-reactive media
* Single or multi–phase fluid flow with or without phase change
* Near–and far–field radiative heat transfer
* Combined modes of heat transfer in complex systems (for example, plasmas, biological, geological,...)
* Multiscale modelling
The applied research topics include:
* Heat exchangers, heat pipes, cooling processes
* Transport phenomena taking place in industrial processes (chemical, food and agricultural, metallurgical, space and aeronautical, automobile industries)
* Nano–and micro–technology for energy, space, biosystems and devices
* Heat transport analysis in advanced systems
* Impact of energy–related processes on environment, and emerging energy systems
The study of thermophysical properties of materials and fluids, thermal measurement techniques, inverse methods, and the developments of experimental methods are within the scope of the International Journal of Thermal Sciences which also covers the modelling, and numerical methods applied to thermal transfer.