Characterization of nanosecond pulse driven dielectric barrier discharge plasma actuators for aerodynamic flow control von Dawson, Robert, Little, Jesse

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Connection Between Flow Structure and Separation Control for Various Fluidic Oscillator Spacings von Otto, Christopher, Little, Jesse C., Woszidlo, Rene

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Momentum Coefficient Governing Discrete Jet Actuation for Separation Control von Otto, Christopher, Little, Jesse C, Rafferty, Bradley, Woszidlo, Rene

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Correction: Transitional Shock Boundary Layer Interactions on a Compression Ramp at Mach 4 von Threadgill, James A. S., Little, Jesse C., Wernz, Stefan H.

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Comparison Between Fluidic Oscillators and Steady Jets for Separation Control von Otto, Christopher, Tewes, Philipp, Little, Jesse C, Woszidlo, Rene

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Volumetric study of a turbulent boundary layer and swept impinging oblique SBLI at Mach 2.3 von Threadgill, James A. S., Little, Jesse C.

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Correction to: Volumetric study of a turbulent boundary layer and swept impinging oblique SBLI at Mach 2.3 von Threadgill, James A. S., Little, Jesse C.

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Post-stall flow control using nanosecond pulse driven dielectric barrier discharge plasma actuators von Little, Jesse, Singh, Ashish, Ashcraft, Timothy, Durasiewicz, Claudia

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An inviscid analysis of swept oblique shock reflections von Threadgill, James A. S., Little, Jesse C.

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High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator von Little, Jesse, Nishihara, Munetake, Adamovich, Igor, Samimy, Mo

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Effects of pulse polarity on nanosecond pulse driven dielectric barrier discharge plasma actuators von Dawson, Robyn A., Little, Jesse

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Parallel vortex body interaction enabled by active flow control von Weingaertner, Andre, Tewes, Philipp, Little, Jesse C.

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Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions von Padmanabhan, Sathyan, Maldonado, Jorge C, Threadgill, James A. S, Little, Jesse C

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Transitional Shock Boundary Layer Interactions on a Compression Ramp at Mach 4 von Threadgill, James A. S, Little, Jesse C, Wernz, Stefan H

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Localized Thermal Perturbations for Control of Turbulent Shear Flows von Little, Jesse

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Effects of Nanosecond Pulse Driven Plasma Actuators on Turbulent Shear Layers von Lehmann, Ralf, Akins, David, Little, Jesse

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End Wall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring—Part II: Validation von Sangston, Keith, Little, Jesse, Lyall, M. Eric, Sondergaard, Rolf

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A comparative study of Ac-dielectric barrier discharge versus Ns-dielectric barrier discharge plasma actuators in an incompressible turbulent mixing layer von Singh, Ashish, Little, Jesse

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Flow Separation Control Using Nanosecond Pulse Driven DBD Plasma Actuators von Rethmel, Chris, Little, Jesse, Takashima, Keisuke, Sinha, Aniruddha, Adamovich, Igor, Samimy, Mo

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Parametric study of Ns-DBD plasma actuators in a turbulent mixing layer von Singh, Ashish, Little, Jesse

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