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...
| المؤلف الرئيسي: | |
|---|---|
| التنسيق: | أطروحة |
| اللغة: | English |
| منشور في: |
2007
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| الموضوعات: | |
| الوصول للمادة أونلاين: | http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf |
| _version_ | 1825828309788786688 |
|---|---|
| author | Rajendran, Parvathy |
| author_facet | Rajendran, Parvathy |
| author_sort | Rajendran, Parvathy |
| collection | USM |
| 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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| first_indexed | 2024-03-06T13:51:42Z |
| format | Thesis |
| id | usm.eprints-8156 |
| institution | Universiti Sains Malaysia |
| language | English |
| last_indexed | 2024-03-06T13:51:42Z |
| publishDate | 2007 |
| record_format | dspace |
| spelling | usm.eprints-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/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf |
| work_keys_str_mv | AT rajendranparvathy mathematicalmodelofcombataircraftsizingperformanceoptimizationtl6712p2762007frb |