header
Image from OpenLibrary

Rim driven thruster optimization using numerical simulation / Yara Omar Hassan Hassan Omar ; Supervised Mohamed Madbouli Abdelrhman , Basman Mohamed Elhadidi

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Yara Omar Hassan Hassan Omar , 2021Description: 68 P . : charts , facsmilies ; 30cmOther title:
  • تحسين أداء الدافع ذو الاطار باستخدام المحاكاه العددية [Added title page title]
Subject(s): Available additional physical forms:
  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: CFD is used to calculate the performance of rim driven thruster. The choice of mesh strategy, turbulence model and cavitation model is validated and veri{uFB01}ed using ITTC benchmark propeller and SeaThrust TM T160 RDT experimental data. Di{uFB00}erent blade parameters are manipulated to test the e{uFB00}ect on thruster performance. Combined cases are applied by adding the vanes with 5-blades rotor and changing pitch angle using 5-blades to enhance efficiency. The later case resulted in the best performance increasing the e{uFB03}ciency by 6:4% and widening the operation range as cavitation is delayed
Tags from this library: No tags from this library for this title. Log in to add tags.
Star ratings
    Average rating: 0.0 (0 votes)
Holdings
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.2021.Ya.R (Browse shelf(Opens below)) Not for loan 01010110083523000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2021.Ya.R (Browse shelf(Opens below)) 83523.CD Not for loan 01020110083523000

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

CFD is used to calculate the performance of rim driven thruster. The choice of mesh strategy, turbulence model and cavitation model is validated and veri{uFB01}ed using ITTC benchmark propeller and SeaThrust TM T160 RDT experimental data. Di{uFB00}erent blade parameters are manipulated to test the e{uFB00}ect on thruster performance. Combined cases are applied by adding the vanes with 5-blades rotor and changing pitch angle using 5-blades to enhance efficiency. The later case resulted in the best performance increasing the e{uFB03}ciency by 6:4% and widening the operation range as cavitation is delayed

Issued also as CD

There are no comments on this title.

to post a comment.