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. Author manuscript; available in PMC: 2014 May 1.
Published in final edited form as: Exp Fluids. 2011 May 1;50(5):1247–1259. doi: 10.1007/s00348-010-0985-y

Figure 11.

Figure 11

Oversmoothing due to the DCT-PLS with a supersonic flow (courtesy of Dr. Kompenhans and Dr. Schroeder, DLR’s institute of aerodynamics and flow technology). A) Raw PIV data. B) PIV velocity field post-processed with the DCT-PLS. C) Difference between the raw and post-processed fields. D) Close-up that reveals the presence of oversmoothing along the shock wave.