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...
Main Author: | Rajendran, Parvathy |
---|---|
Format: | Thesis |
Language: | English |
Published: |
2007
|
Subjects: | |
Online Access: | http://eprints.usm.my/8156/1/MATHEMATICAL_MODEL_OF_COMBAT_AIRCRAFT_SIZING_%26_PERFORMENCE_OPTIMIZATION.pdf |
Similar Items
-
Analysis Of The Suspension Beam In Accelerometer For Stiffness Constant And Resonant Frequency By Using Analytical And Numerical Investigation [TL589.2.A3 W872 2007 f rb].
by: Wong, Wai Chi
Published: (2007) -
Developing A Methodology In Aviation Risk Management Using Susceptibility And Vulnerability Application For Airline Concerning Air Crisis [TL553.5. N576 2007 f rb].
by: Ng, Ying Chow
Published: (2007) -
Flutter Modeling And Simulation Of Wing Section Using Bondgraph Technique [TL574.F6 N841 2005 f rb]
[Microfiche 8089].
by: Abdul Razak, Norizham
Published: (2005) -
Aerodynamic Performance Of USM EFA-1 Remotely Piloted Vehicle [UG1242.D7 Z96 2004 f rb] [Microfiche 7609].
by: Mohd Ali, Zurriati
Published: (2004) -
ESA 343 – AIRCRAFT AERODYNAMICS JANUARY 2014
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2014)