Initial and progressive failure analysis of a composite wing spar structure / Bruce Ralphin Rose.J and Priyadharshini.S
In the present work, a main spar section of a composite wing structure is analyzed for its structural safety in the course of preliminary aircraft design phase. Spar is a spanwise structural member that is used to carry the bending loads and it deals with the self weight of the wing while the airpla...
Saved in:
Main Authors: | Bruce, Ralphin Rose.J, S, Priyadharshini |
---|---|
Format: | Article |
Language: | English |
Published: |
Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM)
2017
|
Subjects: | |
Online Access: | http://ir.uitm.edu.my/id/eprint/21116/1/AJ_Bruce%20Ralphin%20Rose.J%20JME%2017.pdf http://ir.uitm.edu.my/id/eprint/21116/ https://jmeche.uitm.edu.my/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Effect of skin and spar laminate orientations on flutter of composite uav wing
by: Zaki, Nurul Zubaidah, et al.
Published: (2019) -
Building of composite system for Wing using Prepreg
by: Siti Noorkhartina Ishak
Published: (2008) -
Educational software for stress analysis of idealized multi-spar aircraft wing
by: Afiq Safwan, Ahmad Afandi, et al.
Published: (2021) -
The comparison of the exercise stress test tolerance using Bruce and Balke-Ware protocols in Malaysians
by: Jaafar, Zulkarnain, et al.
Published: (2019) -
Tensile properties of kenaf/unsaturated polyester composites filled with a montmorillonite filler
by: Rozman, Haji Din, Prof., et al.
Published: (2011)