Experimental and Numerical Investigation of Active Flow Control of a Serpentine Diffuser
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[1] Mortaza Mani,et al. Predictions of a Supersonic Turbulent Flow in a Square Duct , 2013 .
[2] Michael Amitay,et al. Separation Control in Duct Flows , 2002 .
[3] P. Spalart,et al. Turbulence Modeling in Rotating and Curved Channels: Assessing the Spalart-Shur Correction , 2000 .
[4] J. Callis,et al. Luminescent barometry in wind tunnels , 1990 .
[5] Adam Jirasek,et al. Design of Vortex Generator Flow Control in Inlets , 2006 .
[6] E. Garnier. Flow Control by Pulsed Jet in a Curved S-Duct: A Spectral Analysis , 2015 .
[7] B. A. Reichert,et al. Improving curved subsonic diffuser performance with vortex generators , 1996 .
[8] R. Burdisso,et al. Effectiveness of a Serpentine Inlet Duct Flow Control Technique at Design and Off-Design Simulated Flight Conditions , 2003 .
[9] D. MacManus,et al. Characteristics of unsteady total pressure distortion for a complex aero-engine intake duct , 2018, Aerospace Science and Technology.
[10] P. Spalart. A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .
[11] A. Cary,et al. A Structured and Hybrid-unstructured Grid Euler and Navier-Stokes Solver for General Geometry , 2004 .
[12] Chongam Kim,et al. Adjoint-Based Design Optimization of Vortex Generator in an S-Shaped Subsonic Inlet , 2012 .
[13] J. Callis,et al. Dual-luminophor pressure-sensitive paint: I. Ratio of reference to sensor giving a small temperature dependency , 2003 .
[14] Matthew T. Lakebrink,et al. Numerical Investigation of Fluidic Oscillator Flow Control in an S-Duct Diffuser , 2017 .
[15] Matthew T. Lakebrink,et al. Control of flow distortion in offset diffusers using trapped vorticity , 2019, International Journal of Heat and Fluid Flow.
[16] David G. MacManus,et al. Convoluted Intake Distortion Measurements Using Stereo Particle Image Velocimetry , 2016 .
[17] W. H. Ball. Tests of wall suction and blowing in highly offset diffusers , 1985 .
[18] Andrew J. Dorgan,et al. A Reduced Dissipation Approach for Unsteady Flows on , 2012 .
[19] R. Mathis,et al. Use of zero-net-mass-flow for separation control in diffusing S-duct , 2008 .
[20] Jeffrey W. Hamstra,et al. Active inlet flow control technology demonstration , 2000, The Aeronautical Journal (1968).
[21] B. H. Anderson,et al. Vortex-generator installation studies on steady-state and dynamic distortion , 1996 .
[22] J. Bell,et al. Surface Pressure Measurements Using Luminescent Coatings , 2003 .
[23] J. Peterson,et al. New technique of surface flow visualization based on oxygen quenching of fluorescence , 1980 .
[24] J. Debiève,et al. Effect of air jet vortex generators on a shock wave boundary layer interaction , 2010 .
[25] H. Babinsky,et al. Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions , 2009 .
[26] Bryan Campbell,et al. Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics , 1997 .
[27] D. MacManus,et al. Passive Flow Control Study in an S-Duct Using Stereo Particle Image Velocimetry , 2017 .
[28] R. Burdisso,et al. Effectiveness of a Serpentine Inlet Duct Flow Control Technique at Design and Off-Design Simulated Flight Conditions , 2006 .
[29] B. H. Anderson,et al. Optimal Micro-Vane Flow Control for Compact Air Vehicle Inlets , 2013 .
[30] P. Spalart,et al. A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities , 2006 .
[31] A. C. Brown,et al. Subsonic diffusers designed integrally with vortex generators. , 1968 .
[32] Wing Ng,et al. Active Flow Control of a Boundary Layer-Ingesting Serpentine Inlet Diffuser , 2013 .
[33] Mori Mani,et al. Active "Fail Safe" Micro-Array Flow Control For Advanced Embedded Propulsion Systems , 2009 .
[34] A. Glezer,et al. Control of a Transonic Shock in a Serpentine Diffuser using Surface Fluidic Actuation , 2019, AIAA Aviation 2019 Forum.
[35] Ari Glezer,et al. Distortion Management in a Boundary Layer Ingestion Inlet Diffuser Using Hybrid Flow Control , 2014 .
[36] L. Raja,et al. Control of a Shock/Boundary-Layer Interaction by Using a Pulsed-Plasma Jet Actuator , 2012 .