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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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Bibliographic Details
Main Author: Rajendran, Parvathy
Format: Thesis
Language:English
Published: 2007
Subjects:
TL500-777 Aeronautics. Aeronautical engineering
Online Access:http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf
http://eprints.usm.my/8156/
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id my.usm.eprints.8156
record_format eprints
spelling my.usm.eprints.8156 http://eprints.usm.my/8156/ Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb]. 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 NonPeerReviewed application/pdf en http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf Rajendran, Parvathy (2007) Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb]. Masters thesis, Universiti Sains Malaysia.
institution Universiti Sains Malaysia
building Hamzah Sendut Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Sains Malaysia
content_source USM Institutional Repository
url_provider http://eprints.usm.my/
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
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].
publishDate 2007
url http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf
http://eprints.usm.my/8156/
_version_ 1643700914429624320
score 13.211869

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