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Enhanced UAV conceptual sizing method for optimum design parameters selection / Ahmad Sami Ahmad Ismail Albarawy ; Supervised Mohamed Nader Aboulfotouh

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Ahmad Sami Ahmad Ismail Albarawy , 2020Description: 196 P. : charts , facsimiles ; 30cmOther title:
  • الطريقة المحسنة لاختيار المعاملات المثلى للتصميم التصورى للطائرات بدون طيار [Added title page title]
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  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: 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
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Item type Current library Home library Call number Copy number Status Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2020.Ah.E (Browse shelf(Opens below)) Not for loan 01010110083051000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2020.Ah.E (Browse shelf(Opens below)) 83051.CD Not for loan 01020110083051000

Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering

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

Issued also as CD

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