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...
محفوظ في:
المؤلف الرئيسي: | |
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التنسيق: | أطروحة |
اللغة: | English |
منشور في: |
2007
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الوصول للمادة أونلاين: | http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf |
الوسوم: |
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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.
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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 |