Advanced measuring techniques for supersonic flows

Advanced measuring techniques for supersonic flows  
February 28 – March 3, 2005; M.L. Riethmuller & F. Scarano

Table of contents

• VAN DER DRAAI, R.K - German Dutch Wind Tunnels DNW (EWA), The Netherlands
  Current state of experimental capabilities in high-speed industrial wind tunnels. Conventional measurement techniques vs. advanced non-intrusive techniques
• SCARANO, F.¹; VAN DER DRAAI, R.K.²; VAN SCHINKEL, R.²; TELESCA, A.²; FEENSTRA, G.J.² - ¹TU Delft & ²Dutch Wind Tunnels DNW, The Netherlands
  Design, integration and testing of a PIV system in the industrial supersonic wind tunnel (DNW-SST), lessons learned and perspectives
• LOURENÇO, L.M. – Florida State University, USA
  Particle image velocimetry
• SCHRÖDER, A.; KOMPENHANS, J.; ENGLER, R.; GOLDHAHN, E.- DLR Göttingen, Germany
  Current topics in experimental transonic aerodynamics
• ENGLER, R.H.; HENNE, U.; KLEIN, CHR.; SACHS, W.E. .- DLR Göttingen, Germany
  Pressure sensitive paints in quantitative flow field studies
• WILLERT, C. - German Aerospace Center DLR, Germany
  Doppler global velocimetry: fundamentals, implementation and selected applications
• MEYERS, J.F. - NASA Langley Research Center, USA
  Doppler global velocimetry measurements of supersonic flow fields
• WILLERT, C.¹; LEMPEREUR, CH.²; BARRICAU, PH.²; WERNERT, PH.³ ; MARTINEZ, B.³ - ¹German Aerospace Center DLR, Germany & ²ONERA, France & ³Institut Franco-Allemand de Recherches de Saint-Louis (ISL), France
  Applications of doppler global velocimetry in transonic and supersonic windtunnels
• DAM, N. - Radboud University Nijmegen, The Netherlands
  Molecular tagging velocimetry
• SCARANO, F. - Delft University of Technology, The Netherlands
  PIV image analysis for compressible turbulent flows. Extension of PIV to the hypersonic regime, particle tracers assessment
• SCARANO, F.; ELSINGA, G.E.; VAN OUDHEUSDEN, B.W. - Delft University of Technology, The Netherlands
  Evaluation of aero-optical distortion effects on the accuracy of PIV in compressible flows