[PDF] Experimental and Numerical Investigations of a High Performance Co-Flow Jet Airfoil

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Experimental and Numerical Investigations of a High Performance Co-Flow Jet Airfoil

Abstract:

The work re ected in this thesis includes a detailed study of co- ow jet (CFJ) technologies as they are applied to a typical thin airfoil, NACA 6415, at take-o and landing speeds. Numerical analysis and experimental testing were conducted on baseline and co- ow jet airfoils of the same plan form. The CFJ mechanism employs high pressure air injected along the span at the leading edge while a low pressure source removes the same amount of air along the span at the trailing edge. Hence, the net mass ux of the system is zero energy loss is minimized. The jet produced along the upper surface of the airfoil mixes with and excites the free stream ow resulting in increased lift, augmented stall margin, and decreased drag. At certain angles of attack the decreased drag is negative and thrust is produced. The research was comprised of four phases including computational uid dynamics (CFD) simulations, design and manufacturing of a transformable baseline and adjustable slot size CFJ airfoil, implementation of a CFJ Wind Tunnel Laboratory, and wind tunnel testing.

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