Structural design improvement of unmanned aerial vehicle wing
Almost all engineering systems experience strength versus weight conflict of some description. In the case of airplane wing, there are two primary requirements which must be considered during the structural design process: high strength and stiffness, and lower weight. Due to the restricted nature o...
Saved in:
Main Author: | Kanesan, Gunasegaran |
---|---|
Format: | Thesis |
Language: | English |
Published: |
2014
|
Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/53465/25/GunasegaranKanesanMFKM2014.pdf http://eprints.utm.my/id/eprint/53465/ http://dms.library.utm.my:8080/vital/access/manager/Repository/vital:86591 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Propeller locations study on delta-winged unmanned aerial vehicle (UAV) model
by: Kasim, Khushairi Amri
Published: (2017) -
Design and modeling of portable, economical and high payload unmanned aerial vehicle for aerial surveillance
by: Ban, Sau Keong
Published: (2010) -
Dynamic Load Analysis of the Micro Unmanned Aerial Vehicle (UAV)Structure
by: Mohamad Izham Bin Mohamad Zainal, Mohamad Izham
Published: (2010) -
Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
by: Rashid, Rohayati Ab
Published: (2011) -
Superaugmentation and stability augmentation control system for unmanned aerial vehicle
by: Nogoud, Yasser Abdullah Mahjoub
Published: (2017)