The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad
The study on BWB UAV begins in UiTM in 2005, focused on the design and fundamental aerodynamics and flight dynamics of small Blended Wing-Body (BWB). The objective of this research was to measure the aerodynamic characteristics on BWB Baseline 7 aircraft. It also to analyse pitching, rolling, and ya...
Saved in:
| Main Author: | |
|---|---|
| Format: | Thesis |
| Language: | English |
| Published: |
2019
|
| Online Access: | https://ir.uitm.edu.my/id/eprint/87856/1/87856.pdf https://ir.uitm.edu.my/id/eprint/87856/ |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|