Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Md. Fuad Shah Koslan"'
Autor:
Arvinthan Venugopal, Roslina Mohammad, Md Fuad Shah Koslan, Ashaari Shafie, Alizarin bin Ali, Owi Eugene
Publikováno v:
Metals, Vol 11, Iss 9, p 1453 (2021)
The critical aircraft structure, being the load-bearing members, is a vital component for any aircraft. The effect of fatigue loading, operating conditions, and environmental degradation has caused the structural integrity of the airframe to be asses
Externí odkaz:
https://doaj.org/article/8cb26e88697f4e609706807892959986
Autor:
Jamil Hariz, Othman Mohd Zaid, Wan Mat Wan Ali, Md. Fuad Shah Koslan, Thanakodi Suresh, Ahmad Zaidi Ahmad Mujahid, H. Kamarudin Khairul, Abdullah Shohaimi, Husain Firdaus
Publikováno v:
Materials Science Forum. 819:455-460
A failure characteristic investigation is carried out on a constant forcespring (CFS) (also known as flat spiral spring) fitted in a counterweight balancingmechanism. A SolidWorksSimulation Softwarewas used to performed the static and fatigue test. B
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::57e5b27803800f58548d0a22e4cb720a
https://doi.org/10.4028/www.scientific.net/msf.819.455
https://doi.org/10.4028/www.scientific.net/msf.819.455
Autor:
Md. Fuad Shah Koslan, Ahmad Zaidi Ahmad Mujahid, Gunasilan Manar, Shohaimi Abdullah, Mohd Salleh Bin Mohd Tahir
Publikováno v:
Applied Mechanics and Materials. 471:267-272
The majority of aircrafts structure cracks due to fatigue are thin gage metallic structures and secondary support structures. Beside lower fatigue strength, they may also occur due to mechanical defects, especially at weak area and for areas exposed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7c2bcb7ec4efe1410b848b089dd3952f
https://doi.org/10.4028/www.scientific.net/amm.471.267
https://doi.org/10.4028/www.scientific.net/amm.471.267
Publikováno v:
Materials Science Forum; June 2015, Vol. 819 Issue: 1 p387-392, 6p