Static and dynamic stability of hingeless helicopter blade in hover / Ahmed Abdelmonem Ahmed Hussein ; Supervised Gamal Mohammed Elbayoumi , Samir Mostafa Elkholy
Material type:
TextLanguage: English Publication details: Cairo : Ahmed Abdelmonem Ahmed Hussein , 2015Description: 117 P. : charts ; 30cmOther title: - الاستقرار السكونى و الحركى لريشة طائرة هيليكوبتر لامفصلية أثناء التحويم [Added title page title]
- Issued also as CD
| Item type | Current library | Home library | Call number | Copy number | Status | Barcode | |
|---|---|---|---|---|---|---|---|
Thesis
|
قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2015.Ah.S (Browse shelf(Opens below)) | Not for loan | 01010110068668000 | ||
CD - Rom
|
مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2015.Ah.S (Browse shelf(Opens below)) | 68668.CD | Not for loan | 01020110068668000 |
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.H Helicopter flight trim, stability and control / | Cai01.13.01.M.Sc.2015.Ah.L Low cost framework for parameteridentification of unmanned aerial vehicles / | Cai01.13.01.M.Sc.2015.Ah.L Low cost framework for parameteridentification of unmanned aerial vehicles / | Cai01.13.01.M.Sc.2015.Ah.S Static and dynamic stability of hingeless helicopter blade in hover / | Cai01.13.01.M.Sc.2015.Ah.S Static and dynamic stability of hingeless helicopter blade in hover / | Cai01.13.01.M.Sc.2015.Ah.S Static and dynamic stability of hingeless helicopter blade in hover / | Cai01.13.01.M.Sc.2015.Ah.S Static and dynamic stability of hingeless helicopter blade in hover / |
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
The main objective of the thesis is to investigate the nonlinear geometric effects on the static and dynamic stability of helicopter hingeless rotor in hover. this nonlinearity mainly arises frrm the contribution of the flap and lead-lag bending to the elastic twist. the unsteady aerodynamic model was adapted to include the effect of both the pulsating free stream ans the returning spiral wake. differernt deficiency functions were used; quasi steady C(k) = 1, theodorsen C(k) and lowey C' (k,m.h) both divergence and flutter phenomena were studied
Issued also as CD
There are no comments on this title.
Click on an image to view it in the image viewer