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Improvement of aerodynamic performance of aircraft wing / (Record no. 59934)

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
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.2016.He.I 01010110070878000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.11.Ph.D.2016.He.I 01020110070878000 22.09.2023 CD - Rom 70878.CD