Particle image velocimetry in the crossplane of a supersonic jet in subsonic compressible crossflow.
A particle image velocimetry instrument has been constructed for a transonic wind tunnel and applied to study the interaction created by a supersonic axisymmetric jet exhausting from a flat plate into a subsonic compressible crossflow. Data have been acquired in two configurations; one is a two-dimensional measurement on the streamwise plane along the wind tunnel centerline, and the other is a stereoscopic measurement in the crossplane of the interaction. The presence of the induced counter-rotating vortex pair is clearly visible in both data sets. The streamwise-plane data determined the strength and location of the vortices using the vertical velocity component while the crossplane data directly provided a measurement of the vortical motion. A comparison of the vertical velocity component measured using each configuration showed reasonable agreement.
- Research Organization:
- Sandia National Laboratories (SNL), Albuquerque, NM, and Livermore, CA (United States)
- Sponsoring Organization:
- USDOE
- DOE Contract Number:
- AC04-94AL85000
- OSTI ID:
- 1003904
- Report Number(s):
- SAND2003-2895C; TRN: US201103%%8
- Resource Relation:
- Conference: Proposed for presentation at the 20th International Congress on Instrumentation in Aerospace Simulation Facilities held August 25-29, 2003 in Gottingen, Germany.
- Country of Publication:
- United States
- Language:
- English
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