Thermal Analysis of Cooling Channels on Electromechanical Actuator During Actual Flight-Reference-Cited by-同舟云学术

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Thermal Analysis of Cooling Channels on Electromechanical Actuator During Actual Flight

Published:2022-10 Issue:4 Volume:36 Page:789-802
ISSN:1533-6808
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Gao Zhigang¹,Yang Yuxin²,Zheng Dawen¹,Shang Xiaolong¹,Bai Junhua³,Li Peng¹

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

2. Science and Technology on Combustion, Internal Flow and Thermo-Structure Laboratory, 710025 Xi’an, People’s Republic of China

3. Xi’an Shiyou University, 710065 Xi’an, People’s Republic of China

Funder

Natural Science Basic Research Plan of Shaanxi Province in China

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.T6495

Reference25 articles.

1. PizzarelliM.NasutiF.OnofriM.RoncioniP.VottaR.BattistaF. “Supercritical Methane Heat Transfer Modeling in Rocket Engine Cooling Channels,” AIAA Paper 2013-3995, July 2013, pp. 1–12. 10.2514/6.2013-3995

2. Parametric Analysis of Heat Transfer to Supercritical-Pressure Methane

3. Numerical study of conjugate heat transfer of cryogenic methane in rectangular engine cooling channels at supercritical pressures

4. Heat Transfer Prediction for Methane in Regenerative Cooling Channels with Neural Networks

5. Flow and Mass Transfer of Pyrolytic Aviation Kerosene in Curved Channel

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