Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].

Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].

Tesis ini menerangkan tentang permodelan matematik anggaran berat, prestasi dan pengoptimuman rekabentuk jet pejuang pada tahap konsep awal berasaskan pelbagai kaedah. Model ini dihasilkan khas bagi merekabentuk kapal terbang berinjin kembar yang supersonik untuk operasi “hi-lo-hi”. This thesis g...

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主要作者: Rajendran, Parvathy
格式: Thesis
语言:English
出版: 2007
主题:
TL500-777 Aeronautics
Aeronautical engineering
在线阅读:http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf
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spelling my-usm-ep.81562017-05-31T05:09:01Z Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb]. 2007-04 Rajendran, Parvathy TL500-777 Aeronautics. Aeronautical engineering Tesis ini menerangkan tentang permodelan matematik anggaran berat, prestasi dan pengoptimuman rekabentuk jet pejuang pada tahap konsep awal berasaskan pelbagai kaedah. Model ini dihasilkan khas bagi merekabentuk kapal terbang berinjin kembar yang supersonik untuk operasi “hi-lo-hi”. This thesis gives thorough analysis on the mathematical model of combat aircraft sizing, performance and optimization for initial conceptual design stage, based on various fighter design methodology. The developed mathematical model is specifically for designing a supersonic fighter of twin engine aircraft where the design mission of this fighter is hi-lo-hi operation. 2007-04 Thesis http://eprints.usm.my/8156/ http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf application/pdf en public masters Universiti Sains Malaysia Pusat Pengajian Kejuruteraan Aeroangkasa
institution Universiti Sains Malaysia
collection USM Institutional Repository
language English
topic TL500-777 Aeronautics
Aeronautical engineering
spellingShingle TL500-777 Aeronautics
Aeronautical engineering
Rajendran, Parvathy
Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].
description Tesis ini menerangkan tentang permodelan matematik anggaran berat, prestasi dan pengoptimuman rekabentuk jet pejuang pada tahap konsep awal berasaskan pelbagai kaedah. Model ini dihasilkan khas bagi merekabentuk kapal terbang berinjin kembar yang supersonik untuk operasi “hi-lo-hi”. This thesis gives thorough analysis on the mathematical model of combat aircraft sizing, performance and optimization for initial conceptual design stage, based on various fighter design methodology. The developed mathematical model is specifically for designing a supersonic fighter of twin engine aircraft where the design mission of this fighter is hi-lo-hi operation.
format Thesis
qualification_level Master's degree
author Rajendran, Parvathy
author_facet Rajendran, Parvathy
author_sort Rajendran, Parvathy
title Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].
title_short Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].
title_full Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].
title_fullStr Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].
title_full_unstemmed Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].
title_sort mathematical model of combat aircraft sizing & performance optimization [tl671.2. p276 2007 f rb].
granting_institution Universiti Sains Malaysia
granting_department Pusat Pengajian Kejuruteraan Aeroangkasa
publishDate 2007
url http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf
_version_ 1747819699342671872

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