Abstract
Boundary Layer Ingestion is one of the most trending applications in the aircraft propulsion field. Here, it is applied on a small unmanned aerial vehicle wing to investigate its advantages and disadvantages in terms of lift, drag, power consumption, and propulsive efficiency. To do so, a parametric study is conducted to quantify how these parameters change when the propeller diameter and its horizontal and vertical positions vary.
| Original language | English |
|---|---|
| Title of host publication | NILES 2022 - 4th Novel Intelligent and Leading Emerging Sciences Conference, Proceedings |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 284-287 |
| Number of pages | 4 |
| ISBN (Electronic) | 9781665452410 |
| DOIs | |
| State | Published - 2022 |
| Externally published | Yes |
| Event | 4th Novel Intelligent and Leading Emerging Sciences Conference, NILES 2022 - Giza, Egypt Duration: 22 Oct 2022 → 24 Oct 2022 |
Publication series
| Name | NILES 2022 - 4th Novel Intelligent and Leading Emerging Sciences Conference, Proceedings |
|---|
Conference
| Conference | 4th Novel Intelligent and Leading Emerging Sciences Conference, NILES 2022 |
|---|---|
| Country/Territory | Egypt |
| City | Giza |
| Period | 22/10/22 → 24/10/22 |
Bibliographical note
Publisher Copyright:© 2022 IEEE.
Keywords
- aerodynamics
- BLI
- Boundary Layer Ingestion
- power saving
- propulsion
- UAV
- unmanned aerial vehicle
ASJC Scopus subject areas
- Artificial Intelligence
- Computer Networks and Communications
- Computer Science Applications
- Computer Vision and Pattern Recognition
- Safety, Risk, Reliability and Quality
- Instrumentation
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