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Our main pages on this subject:
| 1. | ONERA - Aérodynamique fondamentale et expérimentale (DAFE) - Publications | | | Benay R., Bourgoing A., Investigation of an asymmetrical Schock-Wave boundary layer interaction in a supersonic planar nozzle.... | | | | 2. | ONERA - Fundamental and Experimental Aerodynamics (DAFE) - Publications | | | Benay R., Bourgoing A., Investigation of an asymmetrical Schock-Wave boundary layer interaction in a supersonic planar nozzle.... | | | | 3. | PSP, Pressure Sensitive Paint, Application to Hypersonics - ONERA / DAFE-EN | | | By using the last images as references, both for calibration and interpretation of the results, we were able to eliminate the consequences of the pyrene evaporation at high temperatures.The map of the pressure field on the central body, equipped with a lateral injection, shows the complexity of the interactions produced by the injection from 24 supersonic nozzles.. | | |
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