Numerical study of aircraft wing anti-icing system using bleed air from turbo-fan engine / (Record no. 78785)

MARC details
000 -LEADER
fixed length control field 02663cam a2200349 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223032630.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 201116s2020 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 Cai01.13.11.M.Sc.2020.Ah.N
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Ahmed Mohamed Mohamed Elsaleh
245 10 - TITLE STATEMENT
Title Numerical study of aircraft wing anti-icing system using bleed air from turbo-fan engine /
Statement of responsibility, etc. Ahmed Mohamed Mohamed Elsaleh ; Supervised Essam E. Khalil , Gamal Abdelmoniem Elhariry , Eslam Said Abdelghany
246 15 - VARYING FORM OF TITLE
Title proper/short title دراسه عدديه لمنع تكوين الثلج على الجناح باستخدام نزيف الهواء من محرك الطائره النفاث
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Ahmed Mohamed Mohamed Elsaleh ,
Date of publication, distribution, etc. 2020
300 ## - PHYSICAL DESCRIPTION
Extent 126 P. :
Other physical details charts , facimiles ;
Dimensions 25cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering
520 ## - SUMMARY, ETC.
Summary, etc. A generally utilized technique in aeronautical industry to overcome icing accretion phenomena is to utilize a bleed hot air for anti-icing system in view of its efficiency and simplicity. In the current work, an anti-icing structure for a usual aircraft wing of NACA 23014 airfoil profile. 3D simulations were done to get the temperature and heat flux distribution on wing outer surface for a constant airplane speed of 0.85 Mach, [2% to 6%] bleed air with high pressure and temperature, [15 to 60 degree] jet impingement angle and [4.5 to 9.01mm] distance between piccolo tube and wing inner surface in order to investigate suitable geometry and mass flow rate for avoiding icing accretion, a performance studding were done on turbofan engine to study effect of bleed air on engine performance parameters. In this research was shown that heated surface on leading edge was increased with jet impingement angle and approaching of piccolo tube to leading edge, by comparing 60-degree jet impingement angle with 15, 30 and 45-degree jet impingement angles, it has been found that heated areas on upper surface increased by 37.7%, 26% and 13% respectively, heated areas on lower surface increased by 36.24%, 25% and 6.2 % respectively
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Aircraft Wing Anti-Icing
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Anti-Icing System
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Bleed Air
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Eslam Said Abdelghany ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Essam E. Khalil ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Gamal Abdelmoniem Elhariry ,
Relator term
856 ## - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="http://172.23.153.220/th.pdf">http://172.23.153.220/th.pdf</a>
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Nazla
Reviser Revisor
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Shimaa
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.M.Sc.2020.Ah.N 01010110082053000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.11.M.Sc.2020.Ah.N 01020110082053000 22.09.2023 CD - Rom 82053.CD
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