Aerodynamics performance of optimal wing profile on MAV wing / Siti Khatijah Hamdan
The optimum design for Micro Air Vehicle (MAV) fixed wing is Zimmerman based on the optimal efficiency, however, the effect of camber to aerodynamics performance on the Zimmerman design are not fully discovered by previous researchers due to wide range of airfoil profile. Thus, the objectives of thi...
Saved in:
| Main Author: | |
|---|---|
| Format: | Student Project |
| Language: | English |
| Published: |
2017
|
| Subjects: | |
| Online Access: | https://ir.uitm.edu.my/id/eprint/53884/1/53884.PDF https://ir.uitm.edu.my/id/eprint/53884/ |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|