Transonic Buffeting Investigation using Unsteady Pressure-Sensitive Paint in a Large Wind Tunnel
Author:
Affiliation:
1. ONERA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1136
Reference17 articles.
1. Klein C., Henne U., Sachs W., Engler R.H., Egami Y., Ondrus V., Beifuss U., Mai H. "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",Int.Congress on Instrumentation in AerospaceSimulation Facilities,ICIASF,Pacific Grove,June10-14,2007.
2. Gregory J.W., Asai K., Kameda M., Liu T., Sullivan J.P. "A Review of Pressure-Sensitive Paint for High-Speed and Unsteady Aerodynamics",proc. IMechE,Vol.222,Part G:J.AerospaceEngineering,2008.
3. Nakakita K.,Arizono H."Visualization ofUnsteadyPressureBehavior of TransonicFlutterusingPressure-SensitivePaint Measurements",27thAppliedAerodynamicsConference,22-25June2009,SanAntonio,Texas,AIAApaper2009-3847.
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