Validation experiment with 4-vortex wake in large tow tank (FAR-Wake Subtask 1.2.2)

Stereo PIV measurements on a 2- and 4-vortex system have been performed in a large tow tank of SVA (Schiffbau-Versuchsanstalt Potsdam GmbH). The considered 4-vortex system consists of two counter-rotating vortex pairs with a span width ratio of b2/b1 = 0.3 and a circulation ratio of Γ2/Γ1 = -0.3. For comparisons also the corresponding 2-vortex system is measured. A submersible Stereo PIV system attached to a vertical traversing system was employed. Cross-sectional velocity fields are obtained of the descending wake vortex system to access the vortex dynamics well into the wake far field. The SVA provided the necessary measurement equipment consisting of a submersible Stereo PIV system, a vertical traversing system and a six component force balance. DLR provided the vortex generator (F13 model), a programmable sequencer unit enabling an adaption of the PIV recording system to the high dynamic range of the velocity fields and defined the test program of the measurement campaign.

[1]  J. D. Crouch,et al.  Instability and transient growth for two trailing-vortex pairs , 1997, Journal of Fluid Mechanics.

[2]  Robert Konrath,et al.  Influence of Renolds number on generation and decay of aircraft wakes: Experimental investigation using generic models, F13 and F13X , 2007 .

[3]  Previous work and present knowledge on vortex instabilities and decay , 2006 .

[4]  H. Vollmers,et al.  INSTABILITY AND UNSTEADINESS OF AIRCRAFT WAKE VORTICES , 2003 .

[5]  Sanjiva K. Lele,et al.  Method for Accelerating the Destruction of Aircraft Wake Vortices , 1998 .

[6]  J. Ortega,et al.  On cooperative instabilities of parallel vortex pairs , 2004, Journal of Fluid Mechanics.

[7]  Jean-Claude Monnier,et al.  Identification of vortex pairs in aircraft wakes from sectional velocity data , 2008 .

[8]  Omer Savas,et al.  Experimental study of the instability of unequal-strength counter-rotating vortex pairs , 2003, Journal of Fluid Mechanics.

[9]  David Fabre,et al.  Unsteadiness, instability and turbulence in trailing vortices , 2005 .

[10]  Thomas Gerz,et al.  Commercial aircraft wake vortices , 2002 .

[11]  Jean-Claude Monnier,et al.  Evaluation of Large-Scale Wing Vortex Wakes from Multi-Camera PIV Measurements in Free-Flight Laboratory , 2007 .

[12]  Christian Willert,et al.  Stereoscopic Digital Particle Image Velocimetry for Application in Wind Tunnel Flows , 1997 .

[13]  T. Gerz,et al.  Two-dimensional wake vortex physics in the stably stratified atmosphere , 1999 .

[14]  Feng Bao,et al.  Experimental study on controlling wake vortex in water towing tank , 2003, 20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03..

[15]  Grégoire Winckelmans,et al.  Vortex methods and their application to trailing wake vortex simulations , 2005 .

[16]  F. Scarano Iterative image deformation methods in PIV , 2002 .

[17]  J. D. Crouch,et al.  Airplane trailing vortices and their control , 2005 .

[18]  Philippe R. Spalart Airplane trailing vortices , 2000 .

[19]  Arnold Tafferner,et al.  Research towards a wake-vortex advisory system for optimal aircraft spacing , 2005 .

[20]  G. Winckelmans,et al.  Previous work and present knowledge on wake vortices near the ground , 2005 .