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Laser velocimeter applications to high-lift researchThe application of the Lockheed-Georgia 2-D laser velocimeter (LV) burst-counter system to the flow field around a 2- and 3-element high-lift airfoil is discussed. The characteristic behavior of the confluent boundary layer (that is, the boundary layer existing downstream of a slot as it approaches and undergoes separation is evaluated. In this application, the LV represents all ideal instruments for nonintrusively probing into the narrow slots and cove areas characterizing mechanical high-lift systems. The work is being performed in the Lockheed-Georgia 10 x 30-inch low-speed test facility using a 9-inch (basic) chord section of the general aviation GAW-1 airfoil. The LV system employs a 4-W argon laser and operates in an off-axis, backscatter mode with a focus length of about 30 inches. Smoke is used as the seeding medium and is injected downstream of the model such that particle uniformity and size are constant upon completion of the tunnel circuit into the test area. The LV system is fully automated by utilizing a MAC-16 minicomputer for positioning, data acquisition, and preliminary data reduction.
Document ID
19820024816
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whipkey, R. R.
(Lockheed-Georgia Co. Marietta, GA, United States)
Jones, G.
(Lockheed-Georgia Co. Marietta, GA, United States)
Braden, J. A.
(Lockheed-Georgia Co. Marietta, GA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1982
Publication Information
Publication: NASA. Langley Research Center Flow Visualization and Laser Velocimetry for Wind Tunnels
Subject Category
Instrumentation And Photography
Accession Number
82N32692
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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