Aerodynamic Analysis of Anti-Armor Missile in Different Flight Modes
碩士 === 國防大學理工學院 === 機械工程碩士班 === 100 === In this research, Computational Fluid Dynamics(CFD) was employed to study the aerodynamic characteristic of lift, drag and stall angle of attack of Javelin missile in different fly modes with Mach number M=0.3~0.5, angle of attack α=0°~5°, the deflection angle...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2012
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| Online Access: | http://ndltd.ncl.edu.tw/handle/75695839754962489449 |