Abstract
Aeroelastic tailoring based on tow-steered composites is applied to the structural design of a horizontal stabiliser. The lift-curve slope of the stabiliser is viewed as the primary performance measure in this work and the aim of the aeroelastic tailoring process is to increase it, with consideration to the stabiliser in a forward, zero or backward-swept configuration. The tow-steered design is compared to a structurally stiff baseline as well as an aeroelastically tailored unidirectional design. It is shown that the use of tow-steered composites can improve the lift-curve slope in all sweep configurations, as well as resulting in designs that can distribute stresses more evenly under load. Furthermore, the tow-steered design enables an additional gain of 3.8% in lift-curve slope beyond the optimal unidirectional ply design.
Original language | English |
---|---|
Title of host publication | International Forum on Aeroelasticity and Structural Dynamics |
Publisher | Curran Associates, Inc |
Pages | 1838-11855 |
Number of pages | 18 |
ISBN (Print) | 9781713871125 |
Publication status | Accepted/In press - 27 May 2022 |
Event | 19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022) - Madrid, Spain Duration: 13 Jun 2022 → 17 Jun 2022 |
Conference
Conference | 19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022) |
---|---|
Abbreviated title | IFASD 2022 |
Country/Territory | Spain |
City | Madrid |
Period | 13/06/22 → 17/06/22 |