Journal with review committee

Prévision de la transition sur une aile en flèche. G. Casalis et D. Arnal. La Recherche Aérospatiale, janvier-février 1990.

Stabilité linéaire de la couche limite par un système d’équations paraboliques. Ch. Airiau et G. Casalis. La Recherche Aérospatiale, septembre-octobre 1993.

Stabilité linéaire et non linéaire de la couche limite laminaire par les Équations de Stabilité Parabolisées. Ch. Airiau et G. Casalis. C.R.A.S. Paris, t. 318, Série II, mai 1994.

Transition laminaire-turbulent de la couche limite. D. Arnal et G. Casalis. La Recherche Aérospatiale, mai-juin 1994.

Linear Stability in Transonic Diffuser Flows. G. Casalis et J. Ch. Robinet. Aerospace, Science and Technology, vol 1, n 1, pp. 37-47, février 1998.

Comparaison d’un calcul de couche limite à forte interaction et d’une solution Navier-Stokes sur une aspérité en régime laminaire stationnaire. C. Roget, J.-Ph. Brazier et G. Casalis. C. R. Acad. des Sciences, Août,1997.

Réceptivité localisée de la couche limite. G. Casalis, C. Gouttenoire et B. Troff. C. R. Acad. des Sciences, Paris, t. 325, Série IIb, Novembre, 1997.

On the practical application of the PSE approach to linear stability analyses. M. Langlois, G. Casalis et D. Arnal. Aerospace, Science and Technology, vol. 2, n 3, Mars-Avril 1998.

Feedback control of the laminar turbulent transition onset in a boundary layer by suction. Ph. Mouyon, G. Casalis, A. Séraudie et S. Prudhomme. Experimental Thermal and Fluid Science, vol. 16, pp. 22-31, 1998.

Spatial instability of planar channel flow with fluid injection through porous walls. G. Casalis, G. Avalon et J. Ph. Pineau. Physics of Fluids, vol. 10, N 10, Octobre 1998.

Shock Oscillations in Diffuser Modeled by a Selective Noise Amplification. J. Ch. Robinet et G. Casalis. AIAA Journal, vol 37, n 4, pp 453-459, April 1999.

Mise en résonance acoustique d’une cavité par l’instabilité naturelle d’un écoulement généré par injection pariétale. F. Vuillot, G. Casalis, G. Avalon et N. Lupoglazoff. C. R. Acad. des Sciences, t. 327, Série II b, pp. 77-83, 1999.

Spatial instability of flow in a semiinfinite cylinder with fluid injection through its porous walls. J. Griffond, G. Casalis, J. Ph. Pineau. European Journal of Mechanics, B/Fluids. Volume 19, issue 1, janvier 2000.

Laminar Turbulent Transition Prediction in Three Dimensional Flow. D. Arnal, G. Casalis. Progress in Aerospace Sciences, vol. 36, issue 2, pp 173-191, Février 2000.

On the dependence on the fomulation of some nonparallel stability applied to the Taylor flow. J. Griffond, G. Casalis. Brief communication dans Physcis of Fluids, février 2000.

Shock wave instability and Carbuncle phenomenon : same intrinsic origin ? J. Ch. Robinet, J. Gressier, G. Casalis, J. M. Moschetta. Journal of Fluids Mechanics , juin 2000.

Critical interaction of a shock wave with an acoustic wave. J. Ch. Robinet, G. Casalis. Physics of Fluids, vol. 13, N 4, Avril 2001.

Boundary layer instability induced by surface suction. P.J. D. Roberts, J.M. Floryan, G. Casalis, D. Arnal. Physics of Fluids, vol. 13, Septembre 2001.

Motor Flow Instabilities, part 2 : Intrinsic linear stability of the flow induced by wall injection. G. Casalis, F. Vuillot. RTO-AVT VKI special course on INTERNAL AERODYNAMICS IN SOLID ROCKET PROPULSION ; May, 27-31, 2002.

Channel flow induced by wall injection of fluid and particles.Th. Feraille, G. Casalis. Physics of Fluids, vol. 15, N 2, Février 2003.

Instabilities and pressure oscillations in solid rocket motors. Y. Fabignon, J. Dupays, G. Avalon, F. Vuillot, N. Lupoglazoff, G. Casalis et M. Prévost. Aerospace Science and Technology, vol. 7, issue 3, pp 191-200, Avril 2003.

Exponential-algebraic transition in the near-field of low supersonic jets. Ch. Millet, G. Casalis. European Journal of Mechanics, B/Fluids, vol. 23 pp 367-379, 2004.

Biglobal linear stability of the flow induced by wall injection. F. Chedevergne, G. Casalis, Th. Féraille. Physics of Fluids, vol. 18, Janvier 2006.

Investigation of the PSE approach for subsonic and supersonic hot jets. Detailed comparisons with LES and Linearized Euler equations results. E. Piot, G. Casalis, F. Muller, Ch. Bailly. Internatioal Journal of Aeroacoustics, vol.5, n. 4, 2006.

Stability of the laminar boundary layer flow encountering a row of roughness elements : Biglobal stability approach and DNS. E. Piot, G. Casalis, U. Rist. European Journal of Mechanics, B/ Fluids, vol. 27, pp 684, 706, 2008.

Absolute stability mechanism of a swept cylinder laminar boundary layer with imposed spanwise periodic boundary conditions. E. Piot, G. Casalis. Physics of Fluids, vol. 21, 2009.

Automatic Transition Predictions Using Simplified Methods. J. Perraud, D. Arnal, G. Casalis, J.-P. Archambaud, Raffaele Donelli. AIAA Journal, vol. 47, No. 11, pp 2676-2684, November 2009.

On the importance of reduced scale Ariane 5 P230 solid rocket motor models in the comprehension and prevention of thrust oscillations. J. Hijlkema, M. Prévost, G. Casalis. CEAS Space Journal, DOI 10.1007/s12567-011-0008-8, Springer, 2011.

Direct numerical simulation and global stability computations of the gaseous motion in solid rocket motors. F. Chedevergne, G. Casalis, J. Majdalani. Journal of Fluid Mechanics, vol. 706, pp 190-218, septembre 2012.

Detailed analysis of the vibration induced instability of a liquid film flow. H. Garih, A. Strzelecki, G. Casalis, J.-L. Estivalèzes. Physics of Fluids, vol. 25, janvier 2013.

Stability and sensitivity analysis in a simplified solid rocket motor flow. G. Boyer, G. Casalis et J.-L. Estivalèzes. Journal of Fluid Mechanics, vol. 722, pp. 618-644, 2013.

Discontinuous Galerkin method for the computation of acoustic modes in led flow ducts with rigid splices. L. Pascal, E. Piot et G. Casalis. Journal of Sound and Vibration, vol. 332, pp. 3270-3288, 2013.

Stability analysis and numerical simulation of simplified solid rocket motors. G. Boyer, G. Casalis, J.-L. Estivalèzes. Physics of Fluids, vol. 25, 2013.

On the transient phase of the Faraday instability. H. Garih, J.-L. Estivalèzes, G. Casalis. Physics of Fluids, 25, 124104, 2013.

On the laminar-turbulent transition in injection-driven porous chambers. B. Gazanion, F. Chedevergne, G. Casalis. Experiments in Fluids, 55:1643, 2014.

Transient ejction phase modeling of a Plasma Synthetic Jet actuator. F. Laurendeau, F. Chedevergne, G. Casalis. Physics of Fluids, vol. 26, 125101, 2014.

Parabolized Stability Equations analysis of nonlinear interactons with forced eigenmodes to control subsonic jet instabilities. M. Itasse, J.-Ph. Brazier, O. Léon et G. Casalis. Physics of Fluids, vol. 27, doi : 10.1063/1.4928472, 2015

Applications of Dielectric Barrier Discharges and Plasma Sythetic Jet Actuators at Onera. F. Chedevergne, G. Casalis, O. Léon, M. Forte, F. Laurendeau, N. Szulga, O. Vermeersch, E. Piot. Journal Aerospace Lab, Plasmas for Aeronautics, Issue 10, Décembre, 2015.

A new Implementation of the Extended Helmholtz Resonator Acoustic Liner Impedance Model in Time Domain CAA. L. Pascal, E. Piot et G. Casalis. Journal of Computational Acoustics, vol 24, Issue 1, March, 2016

Characterization of a highly efficient chevron-shaped anti-contamination device. M. Fiore, O. Vermeersch, M. Forte, G. Casalis, C. François. Experiments in Fluids 57:59 ; DOI 10.1007/s00348-016-2149-1, 2016.