Analysis, Design, Ground and Flight Testing of an Intake System for Transonic Flight

与Atlantis Research Labs Inc.合作，该CRD项目的目标是更好地了解 流动物理与一种新的进气概念相关联，利用这些知识来设计和优化 系统，并执行创新的地面和飞行测试以进行验证。这项工作的动机是 开发用于高速推进应用的亚特兰蒂斯进气系统(AIS)。应用包括 超音速飞机、无人驾驶飞机(UAS)、导弹和目标。最先进的仿真建模技术 将与优化设计结合使用。高马赫数冲量装置将是 与先进的非侵入性诊断技术结合使用，以获得实验验证数据。飞行 测试将涉及飞机的新用途。结果将被用来改进AIS设计，并更好地 了解加热超音速喷流的卷吸作用。这项工作还将提供关于 新型推进循环。除了开发AIS和更好地了解流程 除了物理学，该项目的主要贡献还包括培训高素质人员(HQP)和 增加加拿大西部航空航天领域的高科技研究曝光率。

In collaboration with Atlantis Research Labs Inc., the goals of this CRD project are to better understand the flow physics associated with a novel intake concept, leverage the knowledge to design and optimize the system, and perform innovative ground- and flight-based tests for validation. The work is motivated by the development of the Atlantis Intake System (AIS) for high-speed propulsion applications. Applications include supersonic aircraft, unmanned aerial systems (UAS), missiles, and targets. State-of-the-art simulation modeling will be used in combination with optimization and design. A high Mach number impulse apparatus will be used in conjunction with advanced non-intrusive diagnostics to obtain experimental validation data. Flight testing will involve novel use of aircraft. Results will be exploited to improve the AIS design and better understand entrainment from a heated supersonic jet flow. The work will also provide detailed analysis on a new type of propulsion cycle. In addition to the development of the AIS and better understanding of the flow physics, major contributions from the project also include the training of highly qualified personnel (HQP) and increasing the exposure of high-tech research in the aerospace field in western Canada.