Investigation of Trapped Vorticity Concentrations Effected by Hybrid Actuation in an Offset Diffuser

Trapped vorticity concentration engendered by deliberate modification of the internal surface of an offset diffuser is coupled with a spanwise array of surface-integrated fluidic-oscillating jets for hybrid flow control of the secondary flow that gives rise to flow distortions. The trapped vorticity mimics the effects of local separation within aggressive diffusers and is used as a testbed for investigations of the effectiveness of such hybrid flow control for alleviation the flow distortions at the engine inlet (AIP). The local and global characteristics of the diffuser flow in the absence and presence of the actuation are investigated at Mach numbers up to M = 0.7, using a forty-probe AIP total pressure rake, surface oil-flow visualization, hot-wire anemometry, and particle image velocimetry. The present investigations demonstrate that the actuation affects the strength and scale of the trapped vorticity and its interaction with the cross flow, and consequently alters the flow evolution within the diffuser and leads to significant suppression of pressure distortion at the AIP (by about 80%). These findings indicate that hybrid actuation based on trapped vorticity concentrations can be utilized for mitigation of flow distortion in diffuser flows by strong coupling to the natural formation of vorticity concentrations due to the local flow separation.

[1]  B. H. Anderson,et al.  Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro-Array Actuation , 2006 .

[2]  Ahmad Vakili,et al.  Flow Control In A Diffusing S-Duct , 1985 .

[3]  Michael Amitay,et al.  Separation Control in Duct Flows , 2002 .

[4]  David L. Daggett,et al.  Blended Wing Body Systems Studies: Boundary Layer Ingestion Inlets with Active Flow Control , 2013 .

[5]  Adam Jirasek,et al.  Design of Vortex Generator Flow Control in Inlets , 2006 .

[6]  Mohsen Jahanmiri Active Flow Control , 2012 .

[7]  Robert King Active Flow Control , 2007 .

[8]  Ari Glezer,et al.  Controlled Streamwise Vorticity in Diffuser Boundary Layer using Hybrid Synthetic Jet Actuation , 2009 .

[9]  Michel Stanislas,et al.  Control of a decelerating boundary layer. Part 1: Optimization of passive vortex generators , 2006 .

[10]  B. A. Reichert,et al.  Improving curved subsonic diffuser performance with vortex generators , 1996 .

[11]  Brian G. Allan,et al.  Boundary-Layer-Ingesting Inlet Flow Control , 2013 .

[12]  M. Amitay,et al.  Flow Control in a Diffuser at Transonic Conditions , 2015 .

[13]  Eric Garnier,et al.  Flow Control in a High-Offset Subsonic Air Intake , 2011 .

[14]  M. Amitay,et al.  Effect of boundary layer thickness on secondary structures in a short inlet curved duct , 2013 .

[15]  B. H. Anderson,et al.  Study on vortex generator flow control for the management of inlet distortion , 1993 .

[16]  Alan H. Epstein,et al.  Active Stabilization of Rotating Stall and Surge in a Transonic Single Stage Axial Compressor , 1997 .

[17]  Henry D. Baust,et al.  Management of Total Pressure Recovery, Distortion and High Cycle Fatigue in Compact Air Vehicle Inlets , 2002 .

[18]  Robert Liebeck,et al.  An experimental investigation of boundary layer ingestion in a diffusing S-duct with and without passive flow control , 1999 .

[19]  H. Babinsky,et al.  Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions , 2009 .

[20]  R. Burdisso,et al.  Effectiveness of a Serpentine Inlet Duct Flow Control Technique at Design and Off-Design Simulated Flight Conditions , 2006 .

[21]  Serge Tournier,et al.  Flow analysis and control in a subsonic inlet , 2005 .

[22]  B. H. Anderson,et al.  Optimal Micro-Vane Flow Control for Compact Air Vehicle Inlets , 2013 .

[23]  Joseph D. Vasile,et al.  ACTIVE CONTROL OF INLET DUCTS , 2008 .

[24]  Abraham N. Gissen,et al.  Dynamics of flow control in an emulated boundary layer-ingesting offset diffuser , 2014 .

[25]  Wing Ng,et al.  Active Flow Control of a Boundary Layer-Ingesting Serpentine Inlet Diffuser , 2013 .

[26]  Glenn,et al.  Optimal Micro-Jet Flow Control for Compact Air Vehicle Inlets , 2013 .

[27]  Mori Mani,et al.  Active "Fail Safe" Micro-Array Flow Control For Advanced Embedded Propulsion Systems , 2009 .

[28]  Ari Glezer,et al.  Distortion Management in a Boundary Layer Ingestion Inlet Diffuser Using Hybrid Flow Control , 2014 .