Design of a bladeless engine compressor based on magnetohydrodynamics

Jana Stachová, J. Čerňan
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Abstract

This article is a technical analysis focusing on the design of a bladeless compressor based on magnetohydrodynamics and the possibilities of its use. The aim of this work is to design new solutions in the field of aircraft compressors and to provide a comprehensive overview of scientific information on the topic. Emphasis is also placed on acquainting the reader with the basic principles of magnetohydrodynamics and the possibilities of its application in the field of aircraft propulsion units. The work is a combination of professional research of scientific information in the field of plasma and magnetohydrodynamics and a practical part whose goal is to create new design of a bladeless compressor using scientific observation and modelling methods. This design was also examined in the work using the method of comparison, which aimed to examine the design and its behaviour in different configurations. The main goal was to combine essential and key information from the researched area and apply it in a completely new way in designing new solutions in issued area
基于磁流体力学的无叶片发动机压气机设计
本文对一种基于磁流体力学的无叶片压缩机的设计及其应用的可能性进行了技术分析。这项工作的目的是在飞机压缩机领域设计新的解决方案,并提供有关该主题的科学信息的全面概述。重点还放在使读者熟悉磁流体动力学的基本原理及其在飞机推进装置领域应用的可能性。这项工作结合了等离子体和磁流体动力学领域的科学信息的专业研究和实践部分,其目标是利用科学观察和建模方法创建无叶片压缩机的新设计。该设计也在工作中使用比较方法进行了检查,目的是检查设计及其在不同配置中的行为。主要目标是结合研究领域的基本和关键信息,并以全新的方式应用于设计发布领域的新解决方案
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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