Time domain modeling of unsteady aerodynamic forces on a flapping airfoil

The goal of this research is to develop a versatile and fast code to compute the unsteady lift and thrust forces generated by a flapping airfoil and apply it to engineering problems. We consider both plunging and pitching types of motion and develop a time marching simulation based on early work in unsteady aerodynamics. The ability of the code to compute lift and thrust forces is validated against published results. We then study ways to maximize thrust generation by considering sinusoidal and square motions and optimizing parameters such as flapping frequency, amplitude, and phase difference between pitch and plunge. Finally, the code is applied to the take-off problem of a micro- UAV to illustrate the ability of the code to compute transient forces. The novelty of this research resides in the consideration of square motions and the optimization of parameters to maximize thrust. Also, the ability of the code to show transient forces and yet run faster than real time makes it a valuable tool for a wide variety of applications.

Department dc:contributor.department

Massachusetts Institute of Technology. Department of Aeronautics and Astronautics

Grantor dc:publisher

Massachusetts Institute of Technology

Year dc:date.issued

1998

Author dc:creator

• Durand, Eric, 1973-

Advisor dc:contributor.advisor

• James Paduano.

• Aeronautics and Astronautics

Statement dc:rights

• M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.

Licence dc:rights.uri

• http://dspace.mit.edu/handle/1721.1/7582

Language dc:language.iso

eng

Handle dc:identifier.uri

http://hdl.handle.net/1721.1/47668

OAI identifier oai:identifier

oai:dspace.mit.edu:1721.1/47668