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 |