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Guide for Pressure-Sensitive Paint Testing at NASA Ames Research Center Unitary Plan Wind TunnelOptical measurement techniques have become a standard option for wind tunnel tests. Pressure-sensitive paint (PSP) is a mature test technique and a common experimental technique in many wind tunnels to measure the global mean static pressure on a model. PSP is a valuable tool when a more detailed distribution of the pressure is needed rather than the conventional pressure taps alone. Planning for a test with optical-based techniques can present new challenges even for experienced customer. The purpose of this paper is to provide a resource to the wind tunnel testing community and customers interested in obtaining PSP measurements on a wind tunnel model at the NASA Ames Research Center’s Unitary Plan Wind Tunnel. An overview of PSP mechanics, a list of requirements for ones considering PSP measurements, and PSP deliverable details are specified.
Document ID
20190027089
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Roozeboom, Nettie H.
(NASA Ames Research Center Moffett Field, CA, United States)
Baerny, Jennifer K.
(Jacobs Engineering Group Mountain View, CA, United States)
Date Acquired
July 9, 2019
Publication Date
January 8, 2017
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN77197
ARC-E-DAA-TN35022
Report Number: ARC-E-DAA-TN77197
Report Number: ARC-E-DAA-TN35022
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2018
End Date: January 13, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 147016.03.01.01.11.03
CONTRACT_GRANT: NNA16BD26C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Unitary
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