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Lattice boltzmann method for flow analysis in subsonic axial compressor / Mohammad Ibrahim Mobarak ; Supervised Ibrahim Shabaka , Farouk Owis , Mohamed Hussein

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Mohammad Ibrahim Mobarak , 2018Description: 98 P. : charts , facsimiles ; 30cmOther title:
  • طريقة شبكة بولتزمان لتحليل السريان داخل ضاغط محوري ذي سرعة دون الصوتية [Added title page title]
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  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: In the thesis, a Lattice Boltzmann Model was built and validated for both laminar and turbulent fluid flows with Reynold{u2019}s number ranging from 14,000 to 2,880,000 using a combined LBM Smagorinsky Large Eddy Simulation (LBMLES) Turbulence model and apply it to model flow in turbomachinery. Additionally, the developed LBM model was applied to investigate the flow inside a subsonic axial compressor, innovatively, this is the first time to be achieved in literature using LBM. Finally, the flow field was validated, visualized, and the available turbomachinery parameters were studied for different operating conditions
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Item type Current library Home library Call number Copy number Status Date due Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2018.Mo.L (Browse shelf(Opens below)) Not for loan 01010110077111000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2018.Mo.L (Browse shelf(Opens below)) 77111.CD Not for loan 01020110077111000

Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering

In the thesis, a Lattice Boltzmann Model was built and validated for both laminar and turbulent fluid flows with Reynold{u2019}s number ranging from 14,000 to 2,880,000 using a combined LBM Smagorinsky Large Eddy Simulation (LBMLES) Turbulence model and apply it to model flow in turbomachinery. Additionally, the developed LBM model was applied to investigate the flow inside a subsonic axial compressor, innovatively, this is the first time to be achieved in literature using LBM. Finally, the flow field was validated, visualized, and the available turbomachinery parameters were studied for different operating conditions

Issued also as CD

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