The design of a high aspect ratio HALE aircraft composite wing. part II: buckling and flutter speed analysis / Bambang K. Hadi and IndraPermana
This is the second part on the design of a high aspect ratio HALE-UAV wing using composite materials. The first paper deals only with the static strength analysis. This paper is a continuation of the first paper and presents buckling and flutters analysis. The wing was made of a carbon/epoxy laminat...
Main Authors: | Hadi, Bambang K., Permana, Indra |
---|---|
Format: | Article |
Language: | English |
Published: |
Penerbit UiTM (UiTM Press)
2015
|
Subjects: | |
Online Access: | http://ir.uitm.edu.my/id/eprint/16145/ http://ir.uitm.edu.my/id/eprint/16145/1/AJ_BAMBANG%20K.%20HADI%20JME%2015%20%282%29.pdf |
Similar Items
-
The design of a high aspect ratio HALE aircraft composite wing. part I: static strength analysis / Bambang K. Hadi, Muhammad A. Ghofur and IndraPermana
by: Hadi, Bambang K., et al.
Published: (2015) -
Flutter analysis of supersonic wing with external stores
by: Abdullah, Nur Azam, et al.
Published: (2013) -
Aeroelastic flutter analysis of supersonic wing with multiple external stores
by: Abdullah, Nur Azam, et al.
Published: (2014) -
Numerical simulation of a low aspect ratio wing at low Reynolds number
by: Suliman , M. M. Ali, et al.
Published: (2013) -
Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow
by: Crasta, Asha, et al.
Published: (2016)