Parameters Influencing the Effectiveness of Reaction Control Jets on the Basic Finner

Phillip M. Munday, Kevin C. Massey
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Abstract

Reaction control jets provide a practical option to increase the acceleration rates of high-performance aerodynamic vehicles. Unfortunately, a designer or system engineer incorporating reaction control jets into a design cannot simply add the jet as a point force because it does not account for the change in force due to the modifications of the flowfield caused by the jet. The changes made to the flowfield can impact the forces and moments, enhancing, mitigating, or even reversing the desired force or moment, depending on a complex set of factors. This study examines the influence of different jet configurations, modifications to freestream parameters, and the presence of control surfaces on the body. It is shown that the proximity of the jet to the control surfaces has the most significant impact on the resulting force amplification. The emphasis is placed on differentiating between how the jet interacts with the body and fins. Ultimately, this shows that the interaction with the fuselage is consistent and self-similar, whereas the fins are primarily influenced by the jet blocking the flow and generating a shock that imparts high pressure on the control surface, increasing the force in the direction of the jet.
影响基本芬纳喷气机反作用力控制效果的参数
反作用力控制喷流为提高高性能空气动力飞行器的加速度提供了一种实用的选择。遗憾的是,设计人员或系统工程师在设计中加入反作用力控制喷射器时,不能简单地将喷射器作为一个点力来添加,因为这并没有考虑到喷射器对流场的改变所带来的力的变化。流场的变化会对力和力矩产生影响,增强、减弱甚至逆转所需的力或力矩,这取决于一系列复杂的因素。本研究探讨了不同的喷流配置、自由流参数的修改以及车身控制面的存在所产生的影响。结果表明,射流与控制面的距离对产生的力放大影响最大。重点在于区分射流如何与机身和鳍片相互作用。最终结果表明,喷气与机身的相互作用是一致和自相似的,而与鳍的相互作用则主要受喷气阻塞气流和产生冲击的影响,冲击会对控制面产生高压,从而增加喷气方向的力。
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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