| dc.contributor.author | Michou, Yanick. | |
| dc.contributor.author | Deleglise, Bruno. | |
| dc.contributor.author | Lebrun, Frederic. | |
| dc.contributor.author | Scolan, Emmanuel. | |
| dc.contributor.author | Grivel, Aurélie. | |
| dc.contributor.author | Steiger, Rolf. | |
| dc.contributor.author | Pugin, Raphaël. | |
| dc.contributor.author | Merienne, Marie-Claire. | |
| dc.contributor.author | Le Sant, Yves. | |
| dc.date.accessioned | 2021-12-09T12:46:49Z | |
| dc.date.available | 2021-12-09T12:46:49Z | |
| dc.date.issued | 2015 | |
| dc.identifier.citation | 31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Dallas TX | |
| dc.identifier.uri | https://yoda.csem.ch/handle/20.500.12839/51 | |
| dc.description.abstract | A new unsteady Pressure Sensitive Paint based on a nanostructured sol-gel coating has been developped and tested on a steel model of a civil aircraft in the ONERA's S2MA transonic windtunnel. Two inserts were fitted in the model wing and coated with a sol-gel based nanostructured silica PSP and functionalized by soaking in a Ru(dpp)3 solution. A third insert was prepared with anodised-aluminum PSP for comparison. The test conditions were M = 0.875, PiO = 100 kPa and 185 kPa. Pressure sensitivity of the nanoporous PSP is lower than that of the AA-PSP, however its luminescence intensity is about live times higher than that of the AA-PSP, resulting in a favorable compromise. | |
| dc.subject | pressure sensitive paint,sol-gel,onera,windtunnel,PSP,nanoporous,luminescence | |
| dc.title | Development of a Sol-Gel Based Nanoporous Unsteady Pressure Sensitive Paint and Validation in the Large Transonic Onera S2MA Windtunnel | |
| dc.type | Proceedings Article | |
| dc.type.csemdivisions | Div-T | |
| dc.type.csemresearchareas | Functional Surfaces | |
| dc.identifier.doi | https://arc.aiaa.org/doi/10.2514/6.2015-2408 | |
