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Forced and Moment Measurements with Pressure-Sensitive PaintThe potential of pressure-sensitive paint (PSP) to provide aerodynamic loads measurements has been a driving force behind the development of this measurement technique. To demonstrate the suitability of PSP for this purpose, it is necessary to show that PSP-derived pressures can be accurately integrated over the model surface. This cannot be done simply by demonstrating the accuracy of PSP as compared to pressure taps. PSP errors due to misregistration or temperature sensitivity may be high near model edges, where they will have a strong effect on moment measurements, but where pressure taps are rarely installed. A more suitable technique is to compare integrated PSP data over the entire model surface with balance and/or CFD results. This paper presents results from three experiments in which integrated PSP data is compared with balance and/or CFD data. This allows the usefulness of PSP for force and moment measurements, and by implication for loads measurements, to be assessed.
Document ID
20000103557
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Bell, James H.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Subject Category
Nonmetallic Materials
Meeting Information
Meeting: World Aviation Congress
Location: Burlingame, CA
Country: United States
Start Date: October 19, 1999
End Date: October 21, 1999
Sponsors: American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc.
Funding Number(s)
PROJECT: RTOP 519-20-22
Distribution Limits
Public
Copyright
Other

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