Development of a Sol-Gel Based Nanoporous Unsteady Pressure Sensitive Paint and Validation in the Large Transonic Onera S2MA Windtunnel
Author:
Affiliation:
1. ONERA
2. Swiss Center for Electronics and Microtechnology (CSEM)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2408
Reference11 articles.
1. Application of Pressure-Sensitive Paint for Determination of Dynamic Surface Pressures on a Rotating 65° Delta Wing and an Oscillating 2D profile in Transonic Flow
2. Novel pressure-sensitive paint for cryogenic and unsteady wind tunnel testing
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3. Development of Sprayable Pressure-Sensitive Paint with a Response Time of Less Than 10 μs;AIAA Journal;2019-05
4. Measurement of an Oscillating Shock Wave in a Transonic Flow Using Two Different Pressure Sensitive Paints* (*Ru-based on anodized aluminum vs. Pt-based with screen layer);2018 Aerodynamic Measurement Technology and Ground Testing Conference;2018-06-24
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