Incorporation of Morphing Theory to Aerodynamic Flows
Publication: Journal of Engineering Mechanics
Volume 146, Issue 8
Abstract
The research reported herein makes use of finite-volume simulations of morphing continuum theory (MCT) to reproduce critical relations of thin-airfoil theory for the simple configuration of a flat plate for supersonic and subsonic flows. With a small mesh size of elements, simulations confirm that inviscid flows simulated by MCT match analytic relations for lift and pressure coefficients derived from classical fluid mechanics, a result confirmed by the inviscid MCT equations. Initial success of MCTHyperFOAM version 1.0 for the flat plate indicates that the solver can be extended to more complex aerodynamic flows.
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Acknowledgments
The authors wish to thank the Air Force, the Air Force Institute of Technology (AFIT), and the Oak Ridge Institute for Science and Education (ORISE) for supporting and funding this work. This research was also made possible by collaboration with Dr. James Chen and Mohamad Ibrahim Cheikh at the University of Buffalo and with Mohamed Mohsen Ahmed of the University of Maryland.
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©2020 American Society of Civil Engineers.
History
Received: Oct 14, 2019
Accepted: Mar 4, 2020
Published online: May 28, 2020
Published in print: Aug 1, 2020
Discussion open until: Oct 28, 2020
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