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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Main Author: Rajendran, Parvathy
Format: Thesis
Language:English
Published: 2007
Subjects:
Online Access:http://eprints.usm.my/8156/
http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf
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author Rajendran, Parvathy
author_facet Rajendran, Parvathy
author_sort Rajendran, Parvathy
building USM Institutional Repository
collection Online Access
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
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institution Universiti Sains Malaysia
institution_category Local University
language English
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publishDate 2007
recordtype eprints
repository_type Digital Repository
spelling usm-81562017-05-31T05:09:01Z 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.
spellingShingle TL500-777 Aeronautics. Aeronautical engineering
Rajendran, Parvathy
Mathematical Model Of Combat Aircraft Sizing & Performance Optimization [TL671.2. P276 2007 f rb].
title 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_short 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].
topic TL500-777 Aeronautics. Aeronautical engineering
url http://eprints.usm.my/8156/
http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf