Wind Tunnel Testing Of A Joined-wing Aircraft Model With Additive Manufactured Components

• المؤلفون الرئيسيون: Teo, Zhen Wei, New, Tze How, Ong, Z. A., Nagel, B., Gollnick, V., Pfeiffer, T., Li, S.
• مؤلفون آخرون: School of Mechanical and Aerospace Engineering
• التنسيق: Conference or Workshop Item
• اللغة: English
• منشور في: 2016
• الموضوعات: Additive Manufacturing; Wind Tunnel Testing
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/84550; http://hdl.handle.net/10220/41827

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...