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Three-dimensional laser Doppler anemometer measurements of a jet in a crossflowA three-dimensional laser Doppler anemometer (3D-LDA) was used in a wind tunnel to measure a jet in a crossflow. Measurements were made in the vicinity of a 5-cm-diam jet which issued normally into a 10.65 m/sec wind tunnel crossflow; the velocity ratio Vjet/Vinf was 8. Detailed lateral surveys were made at two elevations (z = cm and 2 cm); both elevations were within the region affected by the boundary layer on the plate. The results are believed to provide reliable velocity field information in the boundary layer of the jet in a crossflow. Turbulence information also is available and believed to be roughly correct, although it may be subject to broadening effects for the lower values of turbulence. A weak vortex pair was observed in the wake at the plate surface. This structure existed in the boundary layer and built confidence because the 3D-LDA was, indeed, able to resolve fine detail in the wake. The capabilities of the 3D-LDA not only allow the making of the velocity surveys, but can be utilized to follow mean streamlines in the flow.
Document ID
19840026624
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Snyder, P.
(NASA Ames Research Center Moffett Field, CA, United States)
Orloff, K. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-85997
NAS 1.15:85997
A-9839
Report Number: NASA-TM-85997
Report Number: NAS 1.15:85997
Report Number: A-9839
Accession Number
84N34695
Funding Number(s)
PROJECT: RTOP 505-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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