Development and Testing of a Wing Morphing Mechanism for the Control of a Swept Wing Tailless Aircraft 2005-01-3391
Inspired by flight in nature, work done by Lippisch, the Hortens, and Northrop offered a chance at achieving the efficiency of bird flight with swept-wing tailless aircraft. Tailless designs have been forced incorporate aerodynamic compromises for control, which have inhibited potential advantages. A morphing mechanism, which changes the twist of wing and can provide pitch, roll and yaw control for a tailless swept wing aircraft. This mechanism is the first step is a series of morphing techniques, which will lead to more fluid, bird-like flight. This research is investigating the design of a morphing wing to improve the flight characteristics of a tailless aircraft. Flight demonstrator and wind-tunnel data is being used to evaluate the stability, control and efficiency of a morphing swept wing tailless aircraft.
Citation: Guiler, R. and Huebsch, W., "Development and Testing of a Wing Morphing Mechanism for the Control of a Swept Wing Tailless Aircraft," SAE Technical Paper 2005-01-3391, 2005, https://doi.org/10.4271/2005-01-3391. Download Citation
Author(s):
Richard Guiler, Wade Huebsch
Affiliated:
West Virginia University, Department of Mechanical and Aerospace Engineering
Pages: 12
Event:
Aerospace Technology Conference and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 2005 Transactions Journal of Aerospace-V114-1
Related Topics:
Aircraft
Wings
Aerodynamics
Pitch
Roll
Yaw
Research and development
Wind tunnel tests
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