全温模拟装置特斯拉型流道的混合效率优化

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-07-28 DOI:10.1016/j.ast.2024.109435
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引用次数: 0

摘要

太空飞行器总温模拟装置将实际气体总温信号引入飞行器开发过程。它可以模拟飞行环境,缩短开发时间,降低总体成本。均匀稳定的温度信号对于精确模拟飞行器的实际飞行速度和高度至关重要。然而,现有的航天飞行器地面测试设施规模庞大,面临着气体混合不够均匀、模拟精度不足等重大挑战。特斯拉流道(Tesla-type flow channel,TFC)因其在不同领域的气体和液体混合中的出色混合能力而得到广泛应用。本文从空间飞行器全温模拟装置的工作原理出发,根据 TFC 的特点,利用 RBF 神经网络响应面和 NSGA-II 算法,提出了一种高混合效率的 TFC 优化设计方法。优化后的 TFC 被应用于全温模拟装置的混合室中,以提高混合效率。这一改进最终提高了在半物理模拟中模拟太空飞行器飞行环境的精度。利用帕累托最优解,最佳压降为 985.50 Pa,温度标准偏差为 39.37 K。这项研究为提高太空飞行器全温度模拟装置的混合性能提供了有价值的参考,同时也满足了在较小的实验室环境中进行全温度模拟的需求。
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Mixing efficiency optimization of Tesla-type flow channel for total temperature simulation device

The space vehicle total temperature simulation device introduces the actual gas total temperature signal into the vehicle development process. It enables the simulation of flight environments, reduces development time, and decreases overall costs. The uniform and stable temperature signal is paramount in accurately simulate the vehicle's real flight speed and altitude. However, the existing ground test facilities for space vehicles, characterized by their large scale, face significant challenges including insufficient uniformity in gas mixing and inadequate simulation accuracy. The Tesla-type flow channel (TFC) is widely applied for its excellent mixing capabilities in gas and liquid mixing across various domains. In this paper, from the working principle of the total temperature simulation device of space vehicle, according to the characteristics of TFC, a high mixing efficiency optimization design method of TFC is proposed by using RBF neural network response surface and NSGA-II algorithm. The optimized TFC is implemented in the mixing chamber of the total temperature simulation device to enhance the mixing efficiency. This improvement ultimately leads to enhanced accuracy in simulating the flight environment of space vehicles during semi-physical simulations. By utilizing the Pareto optimal solution, the optimal pressure drop is 985.50 Pa, while the standard deviation of temperature is 39.37 K. The results demonstrate a significant improvement in mixing efficiency within the total temperature simulation device due to the introduction of the TFC. This study serves as a valuable reference for enhancing the mixing performance of the total temperature simulation device for space vehicles, while also addressing the need for total temperature simulation in smaller laboratory environments.

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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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