header
Image from OpenLibrary

Aerodynamic characteristics and motion simulation of a damaged aircrafat / Yassir Abbas Awad Elkarim Abdalla ; Supervised Mohammed Madbouli Abdelrahman

By: Contributor(s): Material type: TextTextLanguage: eng Publication details: Cairo : Yassir Abbas Awad Elkarim Abdalla , 2009Description: 152P. : charts , facsimiles ; 30cmOther title:
  • الخصائص الايروديناميكية ومحاكاة الحركة لطائرة معطوبة [Added title page title]
Subject(s): Available additional physical forms:
  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: In this thesis panel method is used as a numerical technique . A computer program using Matlab is developed to perform the aerodynamic characteristics and to calculate the aerodynamic coefficients and derivatives as well as the movable control surfaces stability derivatives . The aerodynamics of a damaged aircraft due to the wing fracture horizontal stabilizer fracture aileron fracture elevator fracture and rudder fracture are investigated
Tags from this library: No tags from this library for this title. Log in to add tags.
Star ratings
    Average rating: 0.0 (0 votes)
Holdings
Item type Current library Home library Call number Copy number Status Date due Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2009.Ya.A (Browse shelf(Opens below)) Not for loan 01010110052547000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2009.Ya.A (Browse shelf(Opens below)) 52547.CD Not for loan 01020110052547000

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

In this thesis panel method is used as a numerical technique . A computer program using Matlab is developed to perform the aerodynamic characteristics and to calculate the aerodynamic coefficients and derivatives as well as the movable control surfaces stability derivatives . The aerodynamics of a damaged aircraft due to the wing fracture horizontal stabilizer fracture aileron fracture elevator fracture and rudder fracture are investigated

Issued also as CD

There are no comments on this title.

to post a comment.