@inproceedings{9361e862f79f4563bd1408e64bae640b,
title = "Three Dimensional CFD Analysis of the Sprayed Liquid Flap",
abstract = "Previous studies have reported a novel flow-control technology referred to as the Sprayed Liquid Flap. These previous studies conducted two-dimensional, parametric studies involving the position and strength of an atomized liquid jet emanating from the lower surface of an NACA 0012. The results suggested that the Sprayed Liquid Flap could improve aerodynamic performance in certain conditions. This works aims to expand on these previous studies by investigating the effects of three-dimensional aerodynamics on the Sprayed Liquid Flap using Computational Fluid Dynamics. An attempt is also made to correct two-dimensional Sprayed Liquid Flap aerodynamics for finite wing effects using Lifting Line Theory. The objective of these studies is to understand the effects of finite wing aerodynamics on the Sprayed Liquid Flap and assess the feasibility of its deployment in real-world applications.",
author = "George Loubimov and Douglas Fontes and Michael Kinzel",
note = "Funding Information: The authors acknowledge the University of Central Florida Stokes Advanced Research Computing Center for providing computational resources and support that have contributed to results reported herein. The author G. Loubimov would also like to thank the D.o.D. SMART Fellowship for providing funding for this research. Publisher Copyright: {\textcopyright} 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.; AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 ; Conference date: 03-01-2022 Through 07-01-2022",
year = "2022",
doi = "10.2514/6.2022-1529",
language = "English (US)",
isbn = "9781624106316",
series = "AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA SciTech Forum 2022",
}