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

• Main Authors: Teo, Zhen Wei, New, Tze How, Ong, Z. A., Nagel, B., Gollnick, V., Pfeiffer, T., Li, S.
• Other Authors: School of Mechanical and Aerospace Engineering
• Format: Conference or Workshop Item
• Language: English
• Published: 2016
• Subjects: Additive Manufacturing; Wind Tunnel Testing
• Online Access: https://hdl.handle.net/10356/84550; http://hdl.handle.net/10220/41827
• Institution: Nanyang Technological University

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...