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Enhanced UAV conceptual sizing method for optimum design parameters selection / (Record no. 80246)

MARC details
000 -LEADER
fixed length control field 01835cam a2200325 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223032716.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 210315s2020 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.2020.Ah.E
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Ahmad Sami Ahmad Ismail Albarawy
245 10 - TITLE STATEMENT
Title Enhanced UAV conceptual sizing method for optimum design parameters selection /
Statement of responsibility, etc. Ahmad Sami Ahmad Ismail Albarawy ; Supervised Mohamed Nader Aboulfotouh
246 15 - VARYING FORM OF TITLE
Title proper/short title الطريقة المحسنة لاختيار المعاملات المثلى للتصميم التصورى للطائرات بدون طيار
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Ahmad Sami Ahmad Ismail Albarawy ,
Date of publication, distribution, etc. 2020
300 ## - PHYSICAL DESCRIPTION
Extent 196 P. :
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. This work aims at developing an enhanced conceptual design technique that uses available data to improve design parameters estimation and design point selection.The weight estimation is refined to get betterestimate for take-off weight.The performance matching plot generation is based on the steady performance equations instead of empirical relations from regulations.Optimized performance criteria plots are added to the matching graph to help on the selection of the design. Finally,the wing and tail initial geometry are estimated using some guidelines for selecting the design parameters
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Aircraft Design
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Sizing
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term UAV
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Mohamed Nader Aboulfotouh ,
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 Cai01.13.01.M.Sc.2020.Ah.E 01010110083051000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.M.Sc.2020.Ah.E 01020110083051000 22.09.2023 CD - Rom 83051.CD