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Pressure Sensitive Paint Applied to Flexible Models ProjectOne gap in current pressure-measurement technology is a high-spatial-resolution method for accurately measuring pressures on spatially and temporally varying wind-tunnel models such as Inflatable Aerodynamic Decelerators (IADs), parachutes, and sails. Conventional pressure taps only provide sparse measurements at discrete points and are difficult to integrate with the model structure without altering structural properties. Pressure Sensitive Paint (PSP) provides pressure measurements with high spatial resolution, but its use has been limited to rigid or semi-rigid models. Extending the use of PSP from rigid surfaces to flexible surfaces would allow direct, high-spatial-resolution measurements of the unsteady surface pressure distribution. Once developed, this new capability will be combined with existing stereo photogrammetry methods to simultaneously measure the shape of a dynamically deforming model in a wind tunnel. Presented here are the results and methodology for using PSP on flexible surfaces.
Document ID
20140011261
Acquisition Source
Ames Research Center
Document Type
Other
Authors
Schairer, Edward T.
(NASA Ames Research Center Moffett Field, CA United States)
Kushner, Laura Kathryn
(California Univ. Santa Cruz, CA, United States)
Date Acquired
September 2, 2014
Publication Date
August 1, 2014
Subject Category
Chemistry And Materials (General)
Aeronautics (General)
Report/Patent Number
ARC-E-DAA-TN16126
Report Number: ARC-E-DAA-TN16126
Funding Number(s)
CONTRACT_GRANT: NAS2-03144
WBS: WBS 295670.01.02.27
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
model deformation
pressure sensitive paint
flexible models
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