Using composite materials To fabrication UAV wing
Current trend in aircraft structural design is to use composite material as primary structural elements. The objective of the project is to develop the best way to fabricate aircraft wing using composite material. The best way means the structure must have the best strength to weight ratio. This me...
Main Authors: | Nusyirwan, Istas Fahrurrazi, Dahalan, Md. Nizam |
---|---|
Format: | Monograph |
Language: | English |
Published: |
Universiti Teknologi Malaysia
2003
|
Subjects: | |
Online Access: | http://eprints.utm.my/2686/1/71921.pdf |
Similar Items
-
Software development for aerodynamic characteristics estimation of wing-body combination of aircraft at cubsonic speeds
by: Dahalan, Md. Nizam, et al.
Published: (2001) -
Normal mode finite element analysis of aerofoil wing structure with different materials
by: M. N. A. M., Asri, et al.
Published: (2019) -
Optimal Real Time Evasion against High Speed Pursuer Using Evolutionary Programming
by: Nusyirwan, Istas F., et al.
Published: (2006) -
Development of a Versatile UAV Platform for Agricultural Applications
by: Mohd. Yusof, I., et al.
Published: (2006) -
Determining Potassium Nitrate performance as solid rocket propellant for rocket engine
by: Dahalan, Md. Nizam, et al.
Published: (2003)