| DOI | Resolve DOI: https://doi.org/10.2514/6.2019-2352 |
|---|
| Author | Search for: Fortin, Francois1; Search for: Renaud, Guillaume1; Search for: Roy, Steven1 |
|---|
| Affiliation | - National Research Council Canada. Aerospace
|
|---|
| Format | Text, Article |
|---|
| Conference | AIAA Scitech 2019 Forum, 7-11 January 2019, San Diego, CA, USA |
|---|
| Subject | aviation; computational fluid dynamics; nanocomposites; Cfd approaches; low order; method of moving asymptotes; morphing; optimal shape; optimization approach |
|---|
| Abstract | NRC is developing a technology demonstrator of a stretchable morphing leading edge. Shape optimization of two concepts of droop leading edge was performed using a low-order CFD approach with the Method of Moving Asymptotes optimization approach. A prototype demonstrator was built using the optimal shapes with a novel nanocomposite material and internal mechanism. This paper describes the aerodynamic part of the development. |
|---|
| Publication date | 2019-01-06 |
|---|
| Publisher | American Institute of Aeronautics and Astronautics |
|---|
| In | |
|---|
| Language | English |
|---|
| Peer reviewed | Yes |
|---|
| Export citation | Export as RIS |
|---|
| Report a correction | Report a correction (opens in a new tab) |
|---|
| Record identifier | b25bc054-8f59-478e-ae58-f2326eb6a083 |
|---|
| Record created | 2021-08-24 |
|---|
| Record modified | 2021-08-24 |
|---|
