Aerodynamic Analysis of Javelin Anti-Armor Missile in the Number of Different Wings
碩士 === 國防大學理工學院 === 機械工程碩士班 === 102 === In this research, computational fluid dynamics was applied and low-speed wind tunnel experiments were performed to study the aerodynamic characteristics of lift and drag exhibited by a three-dimensional Javelin antiarmor missile. The missile had various number...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2014
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| Online Access: | http://ndltd.ncl.edu.tw/handle/82666926986788394486 |