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Investigating complex aerodynamic flows with a laser velocimeterThe application of the laser velocimeter in the study of two highly complex aerodynamic flows is discussed. In the first experiment, the laser velocimeter was used with frequency tracking electronics to survey the multiple vortex wake structure behind a model of a large jet transport. The second application is to the study of the induced instantaneous inflow velocities near the blades of a model helicopter rotor; counter-type processing was used in these measurements. In each experiment, the data output channels of these processors were handled in an on-line fashion, including both velocity computations and the plotting of fully reduced data.
Document ID
19770004447
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Orloff, K. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Corsiglia, V. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Biggers, J. C.
(Army Air Mobility Res. and Dev. Lab. Moffett Field, United States)
Ekstedt, T. W.
(Calif. Univ. Davis, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1976
Subject Category
Lasers And Masers
Report/Patent Number
A-6765
NASA-TM-X-73171
Report Number: A-6765
Report Number: NASA-TM-X-73171
Accession Number
77N11390
Funding Number(s)
PROJECT: RTOP 505-10-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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