A study of compressible mixing layers using filtered Rayleigh scatteringHigh Reynolds number compressible planar free shear layers were studied using a planar laser visualization technique. Two convective Mach numbers, M(c) = 0.51 and 0.86, were studied in the developing and fully developed regions. The structures in the M(c) = 0.51 case were characterized by 2D core and roller regions, similar to subsonic shear layers. Also for the M(c) = 0.51 case, plan views in the developing region showed the existence of streamwise streaks, possibly indicating the presence of organized streamwise vorticity. The M(c) = 0.86 flow was much less organized than the lower convective Mach number case and highly three dimensional.
Document ID
19930040985
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Elliott, Gregory S. (NASA Lewis Research Center Cleveland, OH, United States)
Samimy, MO (NASA Lewis Research Center Cleveland, OH, United States)
Arnette, Stephen A. (Ohio State Univ. Columbus, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-0175
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit