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Numerical analysis of an external store separation from a fighter aircraft / (Record no. 56363)

MARC details
000 -LEADER
fixed length control field 01946cam a2200325 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 160510s2015 ua d 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 Cai01.13.11.Ph.D.2015.Al.N
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Alaa Ahmed Mohamed Osman
245 10 - TITLE STATEMENT
Title Numerical analysis of an external store separation from a fighter aircraft /
Statement of responsibility, etc. Alaa Ahmed Mohamed Osman ; Supervised Essam E. Khalil , Osama E. AbdEllatif , Amgad M. Bayoumy
246 15 - VARYING FORM OF TITLE
Title proper/short title التحليل العددي لاسقاط المعلقات الخارجية من طائرة مقاتلة
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Alaa Ahmed Mohamed Osman ,
Date of publication, distribution, etc. 2015
300 ## - PHYSICAL DESCRIPTION
Extent 149 P. :
Other physical details charts ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering
520 ## - SUMMARY, ETC.
Summary, etc. In this thesis, a numerical simulation of a store separating from an aircraft has been studied and validated. A dynamic unstructured tetrahedral mesh approach is used to numerically solving the discretized three dimensional, inviscid and compressible Euler equations. The method used for computations of separation of an external store assuming quasi-steady flow condition. Computations of quasi-steady flow have been directly coupled to a six degree-of-freedom (6DOF) rigid-body motion code to generate store trajectories. Then the trajectory of the store after it's safely separation from the F-16 aircraft till it reaching the Earth's surface are presented and discussedusing MATLAB/Simulink platform
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term CFD Modeling
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Quasi-steady Flow
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Transonic Store Separation
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Amgad M. Bayoumy ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Essam E. Khalil ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Osama E. Abdellatif ,
Relator term
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Aml
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 Cai01.13.11.Ph.D.2015.Al.N 01010110068805000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.11.Ph.D.2015.Al.N 01020110068805000 22.09.2023 CD - Rom 68805.CD