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Conduct overall test operations and evaluate two Doppler systems to detect, track and measure velocities in aircraft wake vorticesA program plan for system evaluation of the two-dimensional Scanning Laser Doppler System (SLDS) is presented. In order to meet system evaluation and optimization objectives the following tests were conducted: (1) noise tests; (2) wind tests; (3) blower flowfield tests; (4) single unit (1-D) flyby tests; and (5) dual unit (2-D) flyby tests. Test results are reported. The final phase of the program included logistics preparation, equipment interface checkouts, and data processing. It is concluded that the SLDS is capable of accurately tracking aircraft wake vortices from small or large aircraft, and in any type of weather.
Document ID
19750007541
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilson, D. J.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Krause, M. C.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Craven, C. E.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Edwards, B. B.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Coffey, E. W.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Huang, C. C.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Jetton, J. L.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Morrison, L. K.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-120600
LMSC-HREC-TR-D390470
Report Number: NASA-CR-120600
Report Number: LMSC-HREC-TR-D390470
Accession Number
75N15613
Funding Number(s)
CONTRACT_GRANT: NAS8-30645
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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