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Abstract
This paper presents an overview of the preliminary design process and findings aimed at morphing of trailing edge (TE) control surfaces for rotorcraft. A design methodology for a camber morphing control surface is presented, although twist can also be induced by applying differential camber of the morphing section span. The concept investigated relies on utilizing conventional aircraft structures and materials for morphing purposes; thus, in essence, has the potential to fulfil the conflicting requirements of lightweight, flexibility and strength at the same time. Based on this concept, the preliminary design work shows that an active trailing edge camber morphing mechanism can be designed after careful considerations of design and actuation requirements. The numerical results presented also indicate that such a morphing scheme increases the 2D aerodynamic efficiency.
Original language | English |
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Title of host publication | AIAA Scitech 2020 Forum |
Subtitle of host publication | 6-10 January 2020, Orlando, FL |
Publisher | American Institute of Aeronautics and Astronautics Inc. (AIAA) |
Pages | 1-13 |
Number of pages | 13 |
ISBN (Electronic) | 978-1-62410-595-1 |
ISBN (Print) | 9781624105951 |
DOIs | |
Publication status | Published - 2020 |
Event | AIAA Scitech 2020 Forum - Orlando, United States Duration: 6 Jan 2020 → 10 Jan 2020 |
Publication series
Name | AIAA Scitech 2020 Forum |
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Volume | 1 PartF |
Conference
Conference | AIAA Scitech 2020 Forum |
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Country/Territory | United States |
City | Orlando |
Period | 6/01/20 → 10/01/20 |
Fingerprint
Dive into the research topics of 'Preliminary Design of a TE Morphing Surface for Rotorcraft'. Together they form a unique fingerprint.Projects
- 1 Finished
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SABRE: Shape Adaptive Blades for Rotorcraft Efficiency
De Breuker, R., Sodja, J. & Zahoor, Y.
1/06/17 → 31/05/21
Project: Research