An experimental study validating the conditions necessary to prevent the formation and ingestion of aero-inlet vortices
The race to create aircraft engines that push the boundaries of efficiency leads to the creation of engines that are not only larger in size, but have lower ground clearances as well. Under certain flow conditions, a surface to inlet vortex may form. These vortices could potentially damage the engin...
主要作者: | Omar Faruq Idris |
---|---|
其他作者: | School of Mechanical and Aerospace Engineering |
格式: | Final Year Project (FYP) |
语言: | English |
出版: |
2014
|
主题: | |
在线阅读: | http://hdl.handle.net/10356/61570 |
相似书籍
-
Two-stream mixing flow with streamwise vorticity
由: Mao, Rong Hai
出版: (2008) -
Aerodynamic data generation and design support for solar UAV : CFD for aircraft loads
由: Muhammad Fursham Mohd Zubir
出版: (2014) -
Improving inlet performance of turbo-ramjet engine by using surface correction
由: Nandhini Raju
出版: (2021) -
An experimental investigation on tapered wings with leading-edge protuberances
由: Ee, Marcus Joon Leng
出版: (2023) -
System identification for longitudinal derivatives for a VTOL UAV
由: Liang, QiYun
出版: (2020)