MARC details
000 -LEADER |
fixed length control field |
01981cam a2200325 a 4500 |
003 - CONTROL NUMBER IDENTIFIER |
control field |
EG-GiCUC |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
170221s2016 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 |
Ph.D |
099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC) |
Classification number |
Cai01.13.11.Ph.D.2016.He.I |
100 0# - MAIN ENTRY--PERSONAL NAME |
Personal name |
Hesham Shahat Mohamed Helal |
245 10 - TITLE STATEMENT |
Title |
Improvement of aerodynamic performance of aircraft wing / |
Statement of responsibility, etc. |
Hesham Shahat Mohamed Helal ; Supervised Essam E. Khalil Hassan , Osama Ezzat Abdellatif , Gamal Abdelmonim Elhariry |
246 15 - VARYING FORM OF TITLE |
Title proper/short title |
تحسين أداء الديناميكا الهوائية لجناح الطائرة |
260 ## - PUBLICATION, DISTRIBUTION, ETC. |
Place of publication, distribution, etc. |
Cairo : |
Name of publisher, distributor, etc. |
Hesham Shahat Mohamed Helal , |
Date of publication, distribution, etc. |
2016 |
300 ## - PHYSICAL DESCRIPTION |
Extent |
157 P. : |
Other physical details |
facsimiles ; |
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. |
Aircraft designers are performing research to improve the overall aircraft efficiency which would be useful both for aircraft manufacturer and airlines. A winglet is a system used to enhance the effectiveness of air plane by increasing lift {u2013}to- drag ratio (L/D).The target of this investigation is compare the aerodynamic characteristics of the wing with and without winglet. For the this study, thesis considered raked winglet with four angles and considered the optimum angle to study the effect of taper ratios and then study blended winglet at four angles, and considered the optimum angle to study the effect of taper ratios, study the effect of length of winglet and Mach number ,using CFD simulation performs by FLUENT ® |
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE |
Additional physical form available note |
Issued also as CD |
653 #4 - INDEX TERM--UNCONTROLLED |
Uncontrolled term |
Aerodynamic Performance |
653 #4 - INDEX TERM--UNCONTROLLED |
Uncontrolled term |
CFD |
653 #4 - INDEX TERM--UNCONTROLLED |
Uncontrolled term |
Winglets |
700 0# - ADDED ENTRY--PERSONAL NAME |
Personal name |
Essam E. Khalil Hassan , |
Relator term |
|
700 0# - ADDED ENTRY--PERSONAL NAME |
Personal name |
Gamal Abdelmonim Elhariry , |
Relator term |
|
700 0# - ADDED ENTRY--PERSONAL NAME |
Personal name |
Osama Ezzat Abdellatif , |
Relator term |
|
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN) |
Cataloger |
Nazla |
Reviser |
Revisor |
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN) |
Cataloger |
Shaima |
Reviser |
Cataloger |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Source of classification or shelving scheme |
Dewey Decimal Classification |
Koha item type |
Thesis |