基于计算流体动力学(CFD)模拟的未知飞机飞行动力学模型(FDM)的开发

A. Loya, S. Arif, M. Arsalan, Siraj Anis, Arsalan Khan, Muhammad Saad Saeed, Abdul Hameed Siddiqui
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引用次数: 1

摘要

计算流体动力学(CFD)的使用在过去十年中增加了10倍,特别是在航空航天科学领域。在本章中,我们将重点讨论如何将插入飞行动力学模型(FDM)的CFD结果与飞机的实际飞行结果进行可行性和有效性的确定。利用实际飞机的飞行数据来确定所设计的FDM的气动性能。除此之外,FDM还包括飞机的各种系统集成;然而,本研究将侧重于气动参数优化。为验证FDM的有效性,进行了相关分析。这将使读者了解CFD如何成为设计未知飞机FDM的伟大工具。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of the Flight Dynamic Model (FDM) Using Computational Fluid Dynamic (CFD) Simulations for an Unknown Aircraft
The usage of computational fluid dynamics (CFD) has enhanced 10-fold since the last decade, especially in the area of aerospace science. In this chapter, we will focus on determining the feasibility and validity of CFD results that are plugged in flight dynamic model (FDM) to that of actual flight of an aircraft. Flight data of an actual aircraft is used to determine the aerodynamic performance of the designed FDM. In addition to this, FDM consist of various systems integration of an aircraft; however, this study will focus on aerodynamic parameter optimization. Relative analysis is carried out to validate the FDM. This will enable readers to know how CFD can be a great tool for designing FDM of an unknown aircraft.
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