An Experimental Study on the Oil Film Method and Pressure of a Missile Body at High-angle-of Attack with Lateral Jet
碩士 === 國立成功大學 === 航空太空工程學系 === 88 === The purpose of the study is to investigate the tangent ogive forebody fineness ratio of 2 at high angle of attack tested in transonic regime. The Mach numbers performed in wind tunnel are 0.3, 0.6, 0.78 and 0.86, respectively, and the corresponding Reynolds numb...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/27477166748145994979 |