Influence of flow injection angle on a leading-edge horseshoe vortex

Abstract Junction flows that develop at the base of protruding obstructions occur in many applications. An unsteady horseshoe vortex is formed as a component of these junction flows, which increases the local heat transfer on the associated endwall. Augmenting this junction flow can be achieved through the injection of fluid upstream of the obstruction. This experimental study evaluated the effects of injection angle for a two-dimensional slot placed upstream of a vane leading-edge with four injection angles of 90°, 65°, 45°, and 30°. Results showed that high momentum injection increased the endwall heat transfer at each slot angle while low momentum injection resulted in a relatively lower augmentation of endwall heat transfer. A leading-edge vortex turning into the endwall was formed at the junction in the stagnation plane for high momentum injection at 90° and 65° while a leading-edge vortex turning away from the wall was formed for 45° and 30° injection. For low momentum injection, a vortex turning into the endwall was formed at all injection angles.

[1]  R. Simpson,et al.  Time-resolved surface heat flux measurements in the wing/body junction vortex , 1993 .

[2]  P. Sagaut,et al.  Flow dynamics past a simplified wing body junction , 2010 .

[3]  이정호,et al.  Fundamentals of Fluid Mechanics, 6th Edition , 2009 .

[4]  R. P. Roy,et al.  Measurements and modeling of the flow and heat transfer in a contoured vane-endwall passage , 2004 .

[5]  F. Pierce,et al.  The Development of a Turbulent Junction Vortex System (Data Bank Contribution) , 1992 .

[6]  T. J. Praisner,et al.  The Dynamics of the Horseshoe Vortex and Associated Endwall Heat Transfer—Part II: Time-Mean Results , 2006 .

[7]  H. Nagamatsu,et al.  Heat transfer in the stagnation region of the junction of a circular cylinder perpendicular to a flat plate , 1986 .

[8]  L. Lourenço Particle Image Velocimetry , 1989 .

[9]  C. Willert,et al.  Digital particle image velocimetry , 1991 .

[10]  Terrence W. Simon,et al.  Heat transfer measurements in a first stage nozzle cascade having endwall contouring: Misalignment and leakage studies , 2006 .

[11]  Satoshi Hada,et al.  The Effect of Leading Edge Diameter on the Horse Shoe Vortex and Endwall Heat Transfer , 2008 .

[12]  T. J. Praisner,et al.  The Dynamics of the Horseshoe Vortex and Associated Endwall Heat Transfer—Part I: Temporal Behavior , 2006 .

[13]  Daniel R. Sabatino,et al.  Boundary Layer Influence on the Unsteady Horseshoe Vortex Flow and Surface Heat Transfer , 2007 .

[14]  Robert J. Moffat,et al.  Describing the Uncertainties in Experimental Results , 1988 .

[15]  Fulvio Scarano,et al.  Advances in iterative multigrid PIV image processing , 2000 .

[16]  K. Thole,et al.  Elevated freestream turbulence effects on heat transfer for a gas turbine vane , 2002 .

[17]  Karen A. Thole,et al.  High Free-Steam Turbulence Effects on Endwall Heat Transfer for a Gas Turbine Stator Vane , 2000 .

[18]  Karen A. Thole,et al.  Effects of Orientation and Position of the Combustor-Turbine Interface on the Cooling of a Vane Endwall , 2012 .

[19]  Karen A. Thole,et al.  Effects of an axisymmetric contoured endwall on a nozzle guide vane: Convective heat transfer measurements , 2010 .

[20]  William J. Devenport,et al.  Turbulence structure near the nose of a wing-body junction , 1987 .

[21]  Axel Dannhauer,et al.  Experimental Investigation of Turbine Leakage Flows on the Three-Dimensional Flow Field and Endwall Heat Transfer , 2007 .

[22]  R. Adrian Particle-Imaging Techniques for Experimental Fluid Mechanics , 1991 .

[23]  Lee S. Langston,et al.  Horseshoe Vortex Formation Around a Cylinder , 1986 .

[24]  Daniel G. Knost,et al.  Heat transfer and film-cooling for the endwall of a first stage turbine vane , 2005 .

[25]  Donald Rockwell,et al.  High image-density particle image velocimetry using laser scanning techniques , 1993 .

[26]  T. V. Jones,et al.  Detailed measurements of heat transfer on and around a pedestal in fully developed passage flow , 1986 .

[27]  Karen A. Thole,et al.  The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane , 2008 .

[28]  Karen A. Thole,et al.  Impact of the Combustor-Turbine Interface Slot Orientation on the Durability of a Nozzle Guide Vane Endwall , 2012 .

[29]  K. Thole,et al.  HEAT TRANSFER AND FLOWFIELD MEASUREMENTS IN THE LEADING EDGE REGION OF A STATOR VANE , 2000 .

[30]  S. C. Dickinson Time dependent flow visualization in the separated region of an appendage-flat plate junction , 2004 .

[31]  Friedrich Kost,et al.  Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I—Aerodynamic Measurements , 2001 .

[32]  W. Terry,et al.  Particle Image Velocimetry , 2009 .

[33]  Martin Nicklas,et al.  Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness , 2001 .

[34]  Karen A. Thole,et al.  Flowfield Measurements in a Single Row of Low Aspect Ratio Pin-Fins , 2012 .

[35]  Karen A. Thole,et al.  Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall , 1999 .

[36]  J. Westerweel Fundamentals of digital particle image velocimetry , 1997 .