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Pressure and Temperature Sensitive Paint Field SystemThis report documents the Pressure and Temperature Sensitive Paint Field System that is used to provide global surface pressure and temperature measurements on models tested in Langley wind tunnels. The system was developed and is maintained by Global Surface Measurements Team personnel of the Data Acquisition and Information Management Branch in the Research Facilities Services Competency. Descriptions of the system hardware and software are presented and operational procedures are detailed.
Document ID
20040065774
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Sprinkle, Danny R. (NASA Langley Research Center Hampton, VA, United States)
Obara, Clifford J. (NASA Langley Research Center Hampton, VA, United States)
Amer, Tahani R. (NASA Langley Research Center Hampton, VA, United States)
Faulcon, Nettie D. (NASA Langley Research Center Hampton, VA, United States)
Carmine, Michael T. (NASA Langley Research Center Hampton, VA, United States)
Burkett, Cecil G. (NASA Langley Research Center Hampton, VA, United States)
Pritchard, Daniel W. (NASA Langley Research Center Hampton, VA, United States)
Oglesby, Donald M. (Swales Aerospace Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2004
Subject Category
Instrumentation And Photography
Report/Patent Number
L-183774
NASA/TM-2004-213020
Report Number: L-183774
Report Number: NASA/TM-2004-213020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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