Low velocity impact behavior of fiber metal laminates structures / Ahmed Nabil Abdelmoteleb ; Supervised Abdelhalim Mohamed Elhabak , Mahmoud Abdelrahman Adly , Nagwa Elzayady
Material type:
- سلوك شرائح الألياف المعدنية المركبة تحت حمل صدمات منخفض السرعة [Added title page title]
- Issued also as CD
Item type | Current library | Home library | Call number | Copy number | Status | Barcode | |
---|---|---|---|---|---|---|---|
![]() |
قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.13.M.Sc.2020.Ah.L (Browse shelf(Opens below)) | Not for loan | 01010110081727000 | ||
![]() |
مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.13.M.Sc.2020.Ah.L (Browse shelf(Opens below)) | 81727.CD | Not for loan | 01020110081727000 |
Browsing المكتبة المركزبة الجديدة - جامعة القاهرة shelves Close shelf browser (Hides shelf browser)
No cover image available | No cover image available | No cover image available | No cover image available | No cover image available | No cover image available | No cover image available | ||
Cai01.13.13.M.Sc.2019.Pe.V A variable inertia vibration energy harvester / | Cai01.13.13.M.Sc.2019.Pe.V A variable inertia vibration energy harvester / | Cai01.13.13.M.Sc.2020.Ah.L Low velocity impact behavior of fiber metal laminates structures / | Cai01.13.13.M.Sc.2020.Ah.L Low velocity impact behavior of fiber metal laminates structures / | Cai01.13.13.M.Sc.2020.Ah.T Tribological and mechanical properties of aluminum matrix reinforced by CNTs / AL₂ O₃ / | Cai01.13.13.M.Sc.2020.Ah.T Tribological and mechanical properties of aluminum matrix reinforced by CNTs / AL₂ O₃ / | Cai01.13.13.M.Sc.2020.AK.A Advanced techniques in mechatronic systems / |
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Mechanical Design and Production
Fiber metal laminates (FMLs) consist of layers of thin metal sheets and fiber-reinforced composite layers bonded together. In this study, two different types of FMLs were manufactured and investigated. Each of them is FML 3/2-(0.4) with base metal aluminum 2024-T3, and with two woven (0/90) type fiber/epoxy laminates for each composite layer. Difference between two types is for fiber type. FMLs were prepared using VAP (Vacuum-Assisted process) as a traditional and low-cost process supported by a distributed weight pressure and vacuum. In order to qualify the manufacturing method and samples, the characterization of these two types of FMLs was verified.This description includes the determination of physical material constituents, tensile testing, bending test, quasi-static indentation test, and low-speed impact test. In order to performing impact test, the low velocity test rig was designed and manufactured according to standards and requirements for drop impact test. Characterization results were compared with theoretical calculations. Failure situations also were discussed
Issued also as CD
There are no comments on this title.