NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Instrumentation in wind tunnelsRequirements in designing instrumentation systems and measurements of various physical quantities in wind tunnels are surveyed. Emphasis is given to sensors used for measuring pressure, temperature, and angle, and the measurements of air turbulence and boundary layers. Instrumentation in wind tunnels require accuracy, fast response, diversity and operational simplicity. Measurements of force, pressure, attitude angle, free flow, pressure distribution, and temperature are illustrated by a table, and a block diagram. The LDV (laser Doppler velocimeter) method for measuring air turbulence and flow velocity and measurement of skin friction and flow fields using laser holograms are discussed. The future potential of these techniques is studied.
Document ID
19860019494
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Takashima, K.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1986
Publication Information
ISSN: 0021-4663
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-78012
NAS 1.15:78012
Report Number: NASA-TM-78012
ISSN: 0021-4663
Report Number: NAS 1.15:78012
Accession Number
86N28966
Funding Number(s)
CONTRACT_GRANT: NASW-4006
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available