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Design optimization of a transonic fan using Navier Stokes equations / (Record no. 51585)

MARC details
000 -LEADER
fixed length control field 02222cam a2200337 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223031246.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 150707s2014 ua dhe 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 Ph.D
099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC)
Classification number Cai01.13.01.Ph.D.2014.Mo.D
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Mohamed Ahmed Mohamed Hussein Aziz
245 10 - TITLE STATEMENT
Title Design optimization of a transonic fan using Navier Stokes equations /
Statement of responsibility, etc. Mohamed Ahmed Mohamed Hussein Aziz ; Supervised Mohamed Madbouli Abdelrahman , Farouk Mohamed Owis
246 15 - VARYING FORM OF TITLE
Title proper/short title التصميم الأمثل لضاغط أسرع من الصوت بإستخدام معادلات نافيير ستوكس
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Mohamed Ahmed Mohamed Hussein Aziz ,
Date of publication, distribution, etc. 2014
300 ## - PHYSICAL DESCRIPTION
Extent 159 P. :
Other physical details charts , facsimiles , plans ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 ## - SUMMARY, ETC.
Summary, etc. A design tool is developed for the preliminary design of transonic compressors using experimental correlations to predict the shock losses, profile losses, deviation angle and the design incidence. The developed tool is used to compute an initial geometry for the numerical simulations. The off design operation of the design shape produced by the preliminary method is performed using the computational fluid dynamics. Then, the design of a transonic fan is optimized using the numerical simulation of the compressible-viscous flow equations and simplex optimization algorithm. The blade geometry is defined in terms of set of geometric groups describing the section chord, stagger angle, staking position, the section thickness and camber distributions. A tip injection flow control technology is applied on the optimized transonic fan rotor in order to enhance the rotor stability parameters
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Axial compressor design
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Shock loss model
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Transonic fan
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Farouk Mohamed Owis ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Mohamed Madbouli Abdelrahman ,
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 Enas
Reviser Cataloger
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Nazla
Reviser Revisor
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 Cai01.13.01.Ph.D.2014.Mo.D 01010110065926000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.Ph.D.2014.Mo.D 01020110065926000 22.09.2023 CD - Rom 65926.CD