Numerical computations of gas turbine combustion products effects on film cooling effectiveness / (Record no. 47712)

MARC details
000 -LEADER
fixed length control field 02014cam a2200337 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223031051.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 141011s2014 ua h 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 Cai01.13.11.M.Sc.2014.Ib.N
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Ibrahim Mohamed Hasan Sayed
245 10 - TITLE STATEMENT
Title Numerical computations of gas turbine combustion products effects on film cooling effectiveness /
Statement of responsibility, etc. Ibrahim Mohamed Hasan Sayed ; Supervised Essam Eldin Khalil , Gamal Abdelmenam Elhariry
246 15 - VARYING FORM OF TITLE
Title proper/short title التحليل العددى لتأثير نواتج أحتراق توربينة غازية على كفاءه التبريد الغشائى
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Ibrahim Mohamed Hasan Sayed ,
Date of publication, distribution, etc. 2014
300 ## - PHYSICAL DESCRIPTION
Extent 122 P. :
Other physical details facsimiles ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering
520 ## - SUMMARY, ETC.
Summary, etc. Cooling technologies for gas turbine applications play an increasingly more important role. This is due to the high firing temperatures to meet the demand for higher performance turbine power. Film cooling is a technique employed to protect the external surface of gas turbine blades from the hot mainstream gas by ejecting the internal coolant air through discrete holes or slots at several locations on the blade exterior surface. Passing the coolant through conventional cylindrical holes causes protection for gas turbine blades from high temperatures. Early studies have proved that the results obtained on simple flat surfaces models can be applied to real engine design with slight corrections
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Effectiveness
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Film cooling
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Turbine
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Essam Eldin Khalil ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Gamal Abdelmenam Elhariry ,
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 Cai01.13.11.M.Sc.2014.Ib.N 01010110063493000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.11.M.Sc.2014.Ib.N 01020110063493000 22.09.2023 CD - Rom 63493.CD
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