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Blade shape optimization of aircraft propeller using space mapping surrogates / (Record no. 71173)

MARC details
000 -LEADER
fixed length control field 02149cam a2200337 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223032236.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 190402s2018 ua dh f m 000 0 eng d
040 ## - CATALOGING SOURCE
Original cataloging agency EG-GiCUC
Language of cataloging eng
Transcribing agency EG-GiCUC
041 0# - LANGUAGE CODE
Language code of text/sound track or separate title eng
049 ## - LOCAL HOLDINGS (OCLC)
Holding library Deposite
097 ## - Thesis Degree
Thesis Level M.Sc
099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC)
Classification number Cai01.13.10.M.Sc.2018.Us.B
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Usama Toson Fouad Toman
245 10 - TITLE STATEMENT
Title Blade shape optimization of aircraft propeller using space mapping surrogates /
Statement of responsibility, etc. Usama Toson Fouad Toman ; Supervised Abdelkareem S. O. Hassan , Farouk M. Owis
246 15 - VARYING FORM OF TITLE
Title proper/short title التصميم الأمثل لشكل ريشة مروحة طائرة باستخدام بدائل تحويلات الفضاء
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Usama Toson Fouad Toman ,
Date of publication, distribution, etc. 2018
300 ## - PHYSICAL DESCRIPTION
Extent 80 P. :
Other physical details charts , facsimiles ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Mathematics and Physics
520 ## - SUMMARY, ETC.
Summary, etc. The aim of the present study is to perform a propeller blade shape optimization for maximum aerodynamic efficiency with a minimal number of high-fidelity model evaluations. A space mapping algorithm is utilized to link two of the most common propeller analysis models: the classical blade element momentum theory to be the coarse model; and the high-fidelity computational fluid dynamics (CFD) tool as the fine model. The optimum design is obtained after few iterations with only 56 CFD simulations. Further, an optimization method based on design of experiments and kriging response surface is used to validate the results and compare the computational efficiency of the two techniques.Finally, the shape of the blade cross-sectional airfoil is optimized to gain an additional improvement of 1.75% in the overall propeller efficiency
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Blade element method
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Computational fluid dynamics
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Propeller design optimization
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Abdelkareem S. O. Hassan ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Farouk M. Owis ,
Relator term
856 ## - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="http://172.23.153.220/th.pdf">http://172.23.153.220/th.pdf</a>
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Nazla
Reviser Revisor
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Shimaa
Reviser Cataloger
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme Dewey Decimal Classification
Koha item type Thesis
Holdings
Source of classification or shelving scheme Not for loan Home library Current library Date acquired Full call number Barcode Date last seen Koha item type Copy number
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة قاعة الرسائل الجامعية - الدور الاول 11.02.2024 Cai01.13.10.M.Sc.2018.Us.B 01010110077519000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.10.M.Sc.2018.Us.B 01020110077519000 22.09.2023 CD - Rom 77519.CD