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Optimization of turbine film cooling using navier stokes equations / (Record no. 50930)

MARC details
000 -LEADER
fixed length control field 02410cam a2200337 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223031228.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 150518s2014 ua eo 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.Ah.O
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Ahmed Mohamed Elsayed Ahmed
245 10 - TITLE STATEMENT
Title Optimization of turbine film cooling using navier stokes equations /
Statement of responsibility, etc. Ahmed Mohamed Elsayed Ahmed ; Supervised Mohamed Madbouli Abdelrahman , Farouk Mohamed Owis
246 15 - VARYING FORM OF TITLE
Title proper/short title التصميم الأمثل للتبريد الغشائى لتوربينة بإستخدام معادلات نافير ستوكس
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Ahmed Mohamed Elsayed Ahmed ,
Date of publication, distribution, etc. 2014
300 ## - PHYSICAL DESCRIPTION
Extent 137 P. :
Other physical details plans , photographs ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 ## - SUMMARY, ETC.
Summary, etc. Over the past fifty years, aircraft and power generation gas turbine designers have focused on increasing the temperature at the combustor exit to improve the engine performance, to increase the thrust and to reduce the fuel consumption. Unfortunately, these high temperatures have a negative effect on the integrity of the high-pressure turbine components and specifically the turbine blades. Therefore, there is a need to have an efficient cooling system engineered in a way such that the maximum blade surface temperature during the engine operation does not exceed the maximum allowable temperature of the blade material. In addition, the tip leakage flow across the turbine blade reduces its aerodynamic performance and causes blade - tip overheating due to this high speed flow and the existence of a thin boundary layer. Film cooling is vital to gas turbine blades to protect them from high temperatures and hence high thermal stresses. In the current study, film cooling on a flat plate is studied numerically to select the different parameters of the compound - hole shape that could enhance the cooling effectiveness
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Blade
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Cooling
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Optimizations
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 Nazla
Reviser Revisor
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Samia
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 Cai01.13.01.Ph.D.2014.Ah.O 01010110065445000 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.Ah.O 01020110065445000 22.09.2023 CD - Rom 65445.CD