Experimental Investigation of Aerodynamics over Transonic Missile Body with Lateral Jet
碩士 === 國立成功大學 === 航空太空工程學系 === 89 === An experimental investigation was conducted in transonic wind tunnel for studying the aerodynamics characteristics due to a lateral jet from an ogive nose missile body having a fineness ratio of 2. The test Mach numbers range from 0.3 to 0.86, the corresponding...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2001
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| Online Access: | http://ndltd.ncl.edu.tw/handle/56740491166035717625 |