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Transonic Flow

Our main pages on this subject:

1.ONERA - Aérodynamique fondamentale et expérimentale (DAFE) - Publications
 Analysis of unsteadiness in afterbody transonic flows....
 
2.ONERA - Fundamental and Experimental Aerodynamics (DAFE) - Publications
 Analysis of unsteadiness in afterbody transonic flows....
 
3.ONERA - Aerodynamics and Energetics Modeling (DMAE) - References
 Calculation of the unsteady transonic flow taking the test section into account...
 
4.Two-component plane PIV at ONERA DAFE - ONERA / DAFE-EN
 Shock-induced separation is a frequently encountered phenomenon in external and internal transonic flows, which may cause detrimental unsteadiness and dramatically reduce the aerodynamical performances of, e.g., an airfoil or an air intake.... References 1 Raffel M., Willert C., Wereley S., Kompenhans J., Particle image velocimetry : a practical guide, Springer-Verlag, 2007. 2 Sartor F., Losfeld G., Bur R., Characterization by PIV of the effect of vortex generators in a transonic separated flow, submitted to the AIAA J....
 
5.Transonic Flow around Fuselage and Wings - ONERA's Science Pictures
 Transonic Flow around Fuselage and Wings - ONERA's Science PicturesWho are we ?Science Pictures... Transonic Flow around Fuselage and Wings copyright © ONERA 1996-2006 - All rights reserved. Computing of the Transonic Flow around Fuselage and Wings for the Cat3D project (Computation by Vincent Brunet -).
 

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