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Numerical analysis of an external store separation from a fighter aircraft / Alaa Ahmed Mohamed Osman ; Supervised Essam E. Khalil , Osama E. AbdEllatif , Amgad M. Bayoumy

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Alaa Ahmed Mohamed Osman , 2015Description: 149 P. : charts ; 30cmOther title:
  • التحليل العددي لاسقاط المعلقات الخارجية من طائرة مقاتلة [Added title page title]
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Dissertation note: Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering Summary: In this thesis, a numerical simulation of a store separating from an aircraft has been studied and validated. A dynamic unstructured tetrahedral mesh approach is used to numerically solving the discretized three dimensional, inviscid and compressible Euler equations. The method used for computations of separation of an external store assuming quasi-steady flow condition. Computations of quasi-steady flow have been directly coupled to a six degree-of-freedom (6DOF) rigid-body motion code to generate store trajectories. Then the trajectory of the store after it's safely separation from the F-16 aircraft till it reaching the Earth's surface are presented and discussedusing MATLAB/Simulink platform
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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 Cai01.13.11.Ph.D.2015.Al.N (Browse shelf(Opens below)) Not for loan 01010110068805000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.11.Ph.D.2015.Al.N (Browse shelf(Opens below)) 68805.CD Not for loan 01020110068805000

Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering

In this thesis, a numerical simulation of a store separating from an aircraft has been studied and validated. A dynamic unstructured tetrahedral mesh approach is used to numerically solving the discretized three dimensional, inviscid and compressible Euler equations. The method used for computations of separation of an external store assuming quasi-steady flow condition. Computations of quasi-steady flow have been directly coupled to a six degree-of-freedom (6DOF) rigid-body motion code to generate store trajectories. Then the trajectory of the store after it's safely separation from the F-16 aircraft till it reaching the Earth's surface are presented and discussedusing MATLAB/Simulink platform

Issued also as CD

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