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Camera Setup for Unsteady Pressure Sensitive Paint at NASA Ames Research CenterThe unsteady Pressure-Sensitive Paint Development Team at NASA Ames Research Center is conducting a Launch Vehicle Demo Test in the Unitary Plan Wind Tunnel’s 11-ft Transonic Wind Tunnel in the first half of 2024 to showcase improvements made to unsteady Pressure-Sensitive Paint technology. The unsteady Pressure-Sensitive Paint setup has upgraded from a four-camera system to an eight-camera system, prompting analysis to maximize the system performance and overall data quality. Additional analysis was performed to maximize the system resolving power when subject to test constraints such as model size and model tunnel positions. These analyses have uncovered new opportunities to improve the unsteady Pressure-Sensitive Paint technology and will allow the system to collect higher quality data with simple changes to the setup procedure.
Document ID
20230016296
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Nicholas Califano
(Metis Technology Solutions, Inc. Albuquerque, NM)
E Lara Lash
(Ames Research Center Mountain View, California, United States)
Nettie H Roozeboom
(Ames Research Center Mountain View, California, United States)
Date Acquired
November 8, 2023
Subject Category
Instrumentation and Photography
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 951888.03.01.03.04.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Camera Calibration
uPSP
LVDT
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