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A laser velocimeter system for large-scale aerodynamic testingA unique laser velocimeter was developed that is capable of sensing two orthogonal velocity components from a variable remote distance of 2.6 to 10 m for use in the 40- by 80-Foot and 80- by 120-Foot Wind Tunnels and the Outdoor Aerodynamic Research Facility at Ames Research Center. The system hardware, positioning instrumentation, and data acquisition equipment are described in detail; system capabilities and limitations are discussed; and expressions for systematic and statistical accuracy are developed. Direct and coupled laboratory measurements taken with the system are compared with measurements taken with a laser velocimeter of higher spatial resolution, and sample data taken in the open circuit exhaust flow of a 1/50-scale model of the 80- by 120-Foot Wind Tunnel are presented.
Document ID
19840008076
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Reinath, M. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Orloff, K. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Snyder, P. K.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
A-9524
NAS 1.15:84393
NASA-TM-84393
Report Number: A-9524
Report Number: NAS 1.15:84393
Report Number: NASA-TM-84393
Accession Number
84N16144
Funding Number(s)
PROJECT: RTOP 505-31-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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