Experimental Study of Shock Oscillation over a Transonic Supercritical Profile

By L. Jacquin, P. Molton, Sébastien Deck, B. Maury, D. Soulevant. 2009

330 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/f30b6188ec89d0e77818d38041ff7cc632f33801

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. P. Meliga
2. A. Garbaruk
3. Denis Sipp
4. O. Marquet
5. A. Barbagallo
6. Clément Mettot
7. A. Travin
8. F. Sartor

In Computational Mechanics

1. Denis Sipp
2. Clément Mettot
3. F. Sartor
4. O. Marquet
5. A. Barbagallo
6. P. Meliga
7. A. Garbaruk
8. J. Crouch

Citations in the corpus

• Origin of transonic buffet on aerofoils (2007, background): “Controlled experiments show a fairly sudden onset of flow unsteadiness as the angle of attack is increased (McDevitt & † Email address for correspondence: jeffrey.d.crouch@boeing.com Okuno 1985; Jacquin et al. 2005).”
• Dynamics and Control of Global Instabilities in Open-Flows: A Linearized Approach (2010, background): “8 and high AoAs, the shock located on the suction side of the wing suddenly starts to oscillate [4], which in turn causes vibrations that are detrimental to the airplane.”
• Predicting the onset of flow unsteadiness based on global instability (2007, background): “The OAT15A airfoil has been investigated by Deck [6] using both URANS and Detached Eddy Simulations (DES).”
• Stability, Receptivity, and Sensitivity Analyses of Buffeting Transonic Flow over a Profile (2015, result): “[28] is considered as a reference experimental case and is used to compare the results.”