MARC details
| 000 -LEADER |
|---|
| fixed length control field |
01748cam a2200313 a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
|---|
| control field |
EG-GiCUC |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
100617s2010 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.2010.Mo.D |
| 100 0# - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Mohamed Ahmed Mohamed Hussein Aziz |
| 245 10 - TITLE STATEMENT |
|---|
| Title |
Design optimization of a three dimensional supersonic intake / |
| Statement of responsibility, etc. |
Mohamed Ahmed Mohamed Hussein Aziz ; Supervised Mohamed Madbouli Abdelrahman , Hesham Mahmoud Elbanna |
| 246 15 - VARYING FORM OF TITLE |
|---|
| Title proper/short title |
الحصول على التصميم الأمثل لمدخل الهواء للطائرات فائقة السرعة |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
|---|
| Place of publication, distribution, etc. |
Cairo : |
| Name of publisher, distributor, etc. |
Mohamed Ahmed Mohamed Hussein Aziz , |
| Date of publication, distribution, etc. |
2010 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
203P. : |
| 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. |
In this thesis a computer program using Matlab and Python are developed to perform an optimization cycle to design an air intake for supersonic aircraft . First a preliminarily design step this is carried out by calculating Mach number air angles and pressures distributions along the intake . Second a high fidelity design optimization step by using the result of step one and computational fluid dynamics programs (CFD - RC package ) and utilize the simplex algorithm inside the package to obtain the optimun design |
| 530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE |
|---|
| Additional physical form available note |
Issued also as CD |
| 653 #4 - INDEX TERM--UNCONTROLLED |
|---|
| Uncontrolled term |
Air intake |
| 653 #4 - INDEX TERM--UNCONTROLLED |
|---|
| Uncontrolled term |
Optimum design |
| 653 #4 - INDEX TERM--UNCONTROLLED |
|---|
| Uncontrolled term |
Supersonic aircraft |
| 700 0# - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Hesham Mahmoud Elbanna , |
| Relator term |
|
| 700 0# - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Mohamed Madbouli Abdelrahman , |
| Relator term |
|
| 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 |
