Wind Tunnel Testing Of A Joined-wing Aircraft Model With Additive Manufactured Components
In this paper, the suitability of using additive manufacturing to fabricate aircraft test model components for use in wind tunnel testing will be reported. The purpose is to investigate the aerodynamic performance of a joined-wing aircraft model under subsonic flow conditions. The resulting test mo...
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Main Authors: | , , , , , , |
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其他作者: | |
格式: | Conference or Workshop Item |
語言: | English |
出版: |
2016
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主題: | |
在線閱讀: | https://hdl.handle.net/10356/84550 http://hdl.handle.net/10220/41827 |
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機構: | Nanyang Technological University |
語言: | English |