Analysis of alocally manufactured ventis 20 - 100WT HAWT / Mahmoud Mohamed Shawky ; Supervised Mohamed Tawfeek , Basman Elhadidi
Material type:
- المصنعة محليا Ventis 20 - 100WT دراسة الأحمال على التوربينة الأفقية [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 | Cai01.13.01.M.Sc.2015.Ma.A (Browse shelf(Opens below)) | Not for loan | 01010110066971000 | ||
![]() |
مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2015.Ma.A (Browse shelf(Opens below)) | 66971.CD | Not for loan | 01020110066971000 |
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 | ||
Cai01.13.01.M.Sc.2015.Ah.S Static and dynamic stability of hingeless helicopter blade in hover / | Cai01.13.01.M.Sc.2015.Ha.A Application of partial blade pitch for power regulation of HAWT / | Cai01.13.01.M.Sc.2015.Ha.A Application of partial blade pitch for power regulation of HAWT / | Cai01.13.01.M.Sc.2015.Ma.A Analysis of alocally manufactured ventis 20 - 100WT HAWT / | Cai01.13.01.M.Sc.2015.Ma.A Analysis of alocally manufactured ventis 20 - 100WT HAWT / | Cai01.13.01.M.Sc.2015.Ma.E Estimation of the elastic properties of carbon nanotube reinforced composites with damaged nanotubes and material cracks / | Cai01.13.01.M.Sc.2015.Ma.E Estimation of the elastic properties of carbon nanotube reinforced composites with damaged nanotubes and material cracks / |
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
The ventis 20 - 100WT turbine is operated in wind farms in hurghada. The blades were locally manufactured because of the multiple failures and lack of spare parts at the AOI. Here in this thesis, the re - designed blades are aerodynamically and structurally examined. First, the steady and unsteady aerodynamic loads are computed using BEM theory. The structural properties of the 10m composite blade are then obtained from NREL dedicated HAWT software PreComp. The steady loads are computed using NREL software and compared to a FEM, and agree reasonably well. The dynamic loads are then analyzed to determine the fatigue life and that the blades operating at frequencies other than the resonant modes. The fatigue analysis suggests that the re -designed blades have a short life about (70 month at operating RPM). Furthermore, results from an environmental study suggest that the blades life will be shorter about (52 month). In future plan we will test experimentally the manufactured blade locally to meet the design constraints requirements and try to optimize it and find a solution for isolating the material used from the environmental effect
Issued also as CD
There are no comments on this title.