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A probabilistic methodology for radar cross section prediction in conceptual aircraft design.

机译:概念飞机设计中雷达横截面预测的概率方法。

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System effectiveness has increasingly become the prime metric for the evaluation of military aircraft. As such, it is the decision maker's/designer's goal to maximize system effectiveness. Industry and government research documents indicate that all future military aircraft will incorporate signature reduction as an attempt to improve system effectiveness and reduce the cost of attrition. Today's operating environments demand low observable aircraft which are able to reliably take out valuable, time critical targets. Thus it is desirable to be able to design vehicles that are balanced for increased effectiveness.; Previous studies have shown that shaping of the vehicle is one of the most important contributors to radar cross section, a measure of radar signature, and must be considered from the very beginning of the design process. Radar cross section estimation should be incorporated into conceptual design to develop more capable systems. This research strives to meet these needs by developing a conceptual design tool that predicts radar cross section for parametric geometries. This tool predicts the absolute radar cross section of the vehicle as well as the impact of geometry changes, allowing for the simultaneous tradeoff of the aerodynamic, performance, and cost characteristics of the vehicle with the radar cross section. Furthermore, this tool can be linked to a campaign theater analysis code to demonstrate the changes in system and system of system effectiveness due to changes in aircraft geometry.; A general methodology was developed and implemented and sample computer codes applied to prototype the proposed process. Studies utilizing this radar cross section tool were subsequently performed to demonstrate the capabilities of this method and show the impact that various inputs have on the outputs of these models. The F/A-18 aircraft configuration was chosen as a case study vehicle to perform a design space exercise and to investigate the relative impact of shaping parameters on radar cross section. Finally, two unique low observable configurations were analyzed to examine the impact of shaping for stealthiness.
机译:系统有效性已日益成为评估军用飞机的主要指标。因此,最大化系统有效性是决策者/设计者的目标。行业和政府研究文件表明,所有未来的军用飞机都将采用减少签名的方法,以提高系统效率并降低损耗成本。当今的运行环境要求低可观测的飞机,这些飞机能够可靠地取出宝贵的,时间紧迫的目标。因此,期望能够设计出平衡的车辆以提高效率。先前的研究表明,车辆的外形是雷达截面最重要的因素之一,雷达截面是衡量雷达信号的指标,必须从设计过程的一开始就加以考虑。雷达截面估计应纳入概念设计中,以开发功能更强大的系统。这项研究通过开发一种概念设计工具来努力满足这些需求,该工具可以预测雷达几何参数的横截面。该工具可预测车辆的绝对雷达横截面以及几何形状变化的影响,从而可以同时权衡具有雷达横截面的车辆的空气动力学,性能和成本特性。此外,该工具可以链接到战区分析代码,以证明由于飞机几何形状的变化而引起的系统和系统有效性的变化。开发并实施了一种通用方法,并使用了示例计算机代码来对提议的过程进行原型设计。随后进行了使用该雷达横截面工具的研究,以证明该方法的功能并显示各种输入对这些模型的输出的影响。选择F / A-18飞机配置作为案例研究车辆,以进行设计太空演习并研究成形参数对雷达横截面的相对影响。最后,分析了两个独特的低可见性配置,以检查成形对隐身性的影响。

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