Airborne Collision Severity Evaluation - Engine Ingestion
| 项目名称： | Airborne Collision Severity Evaluation - Engine Ingestion |
| 摘要： | The research goal for this project is to better understand the interaction of a fan and UAV during an ingestion scenario. The objectives of this research are to: (i) create a generic high bypass ratio fan model that has features that are representative of a fan in a modern engine typically found on a large commercial transport; (ii) develop a component and full scale validated model of a quadcopter UAV (initially validated critical components in the first phase of the airborne collision research at different conditions) at the conditions of the ingestion event; and (iii) simulate various ingestion events to understand the sensitivity of a collision to various parameters of the ingestion. |
| 状态： | Active |
| 资助组织： | Federal Aviation Administration |
| 开始时间： | 20180830 |
| 预计完成日期： | 0 |
| 实际结束时间： | 0 |
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