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Numerical analysis of turbulent chemically reacting flows in scramjet engines using point-implicit finite-volume scheme / (Record no. 22297)

MARC details
000 -LEADER
fixed length control field 01904nam a2200337 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 090616s2009 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 Cai01.13.01.M.Sc.2009.Mo.N
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Mohammed Sayed Saleh Elsayed Kamel
245 10 - TITLE STATEMENT
Title Numerical analysis of turbulent chemically reacting flows in scramjet engines using point-implicit finite-volume scheme /
Statement of responsibility, etc. Mohammed Sayed Saleh Elsayed Kamel ; Supervised Ali A. Hashem , Farouk M. Owis , Moumen M. Idris
246 15 - VARYING FORM OF TITLE
Title proper/short title التحليل العددى للسريان المضطرب المتفاعل كيميائيا فى المحركات الصدمية فوق الصوتية باستخدام طريقة الاحجام المحدودة اللاضمنية النقطية
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Mohammed Sayed Saleh Elsayed Kamel ,
Date of publication, distribution, etc. 2009
300 ## - PHYSICAL DESCRIPTION
Extent 159P. :
Other physical details charts , facsimiles ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 ## - SUMMARY, ETC.
Summary, etc. This study investigates the steady state two-dimensional flow in scramjet combustors.The flow is modeled by RANS approach,where chemical kinetics model is applied to compute the finite rates of chemical reactions due to the small residence time of species inside engine.Turbulence is modeled based on Boussinesq's assumption,using the Baldwin-Lomax algebraic model,taking into account Degani and Schiff modifications
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Computional Fluid Dynamics
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Finite Volume
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Scramjet Engine
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Ali Abdelfatah Hashem ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Farouk Mohamed Owis ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Moumen Mohamed Idris ,
Relator term
902 ## - LOCAL DATA ELEMENT B, LDB (RLIN)
No. of Items 1
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Fatma
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.M.Sc.2009.Mo.N 01010110051157000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.M.Sc.2009.Mo.N 01020110051157000 22.09.2023 CD - Rom 51157.CD