Conferences with proceedings

Experimental and theoretical analysis of natural transition on "infinite" swept wing. D. Arnal, G. Casalis et J. Cl. Juillen. IUTAM Symposium Laminar-Turbulent Transition, Toulouse, septembre 1989.

Receptivity by Direct Numerical Simulation. G. Casalis et B. Cantaloube. Direct and Large-Eddy Simulation, first ERCOFTAC Workshop, Guildford, Angleterre, Kluwer Academic Publishers, mars 1994.

Weakly non linear instability of the laminar boundary layer calculated by a parabolic system of equations. Ch. Airiau et G. Casalis. "Asymptotic Modelling in Fluid Mechanics", colloque organisé en l’honneur du Professeur Guiraud, Paris, ed. Springer-Verlag, avril 1994.

A survey of the transition prediction methods : from analytical criteria to PSE and DNS. D. Arnal, G. Casalis et J. Cl. Juillen. IUTAM Symposium on Laminar-Turbulent Transition, Sendaï, Japon, Springer-Verlag, septembre 1994.

Non linear PSE compared with DNS and experiment. Ch. Airiau et G. Casalis. IUTAM Symposium on Laminar-Turbulent Transition, Sendaï, Japon, Springer-Verlag, septembre 1994.

Stability and Transition Computation for Complex Basic Flows. D. Arnal, G. Casalis, Ch. Airiau et F. Cazenave. Congrès ICAS’94, Anaheim, U.S.A., septembre 1994.

Nonlinear Stability Analysis with PSE approach. G. Casalis, M.L. Copie, Ch. Airiau et D. Arnal. IUTAM symposium : Nonlinear Instability and Transition in 3D Boundary Layers, Manchester, Angleterre, Kluwer ed., juillet 1995.

Laminar-Turbulent Transiton Boundary Layers : research and applications in France. D. Arnal, G. Casalis, J. Reneaux et J. Cousteix. 28th AIAA Fluid Dynamics Conference, Snowmass, Colorado, USA, 29 juin - 2 juillet (1997).

DNS investigation of leading edge and localized receptivity. G. Casalis, C. Gouttenoire et B. Troff. First AFOSR International Conference on DNS/LES. Louisiana Tech. Univ., Ruston, Louisiana, USA, 4-8 août (1997).

A detailed comparison of non-parallel stability results with experimental data. M. Langlois, P. Mac Donald, G. Casalis, Ch . Masson, I. Paraschivoiu. AIAA 98-0335, Reno, 12-15 Janvier 1998.

Flow instabilities and acoustic resonance of channels with wall injection. G. Avalon, G. Casalis et J. Griffond. 34th AIAA/ASME/SAE/ASEE Conf. Cleveland, OH, 13-15 Juillet 1998.

Self-sustained oscillations in diffusers : modelling and prediction. J. Ch. Robinet et G. Casalis. AIAA paper 98-3419, 34th AIAA/ASME/SAE/ASEE Conf. Cleveland, OH, 13-15 Juillet 1998.

Secondary instability of the planar Taylor flow. J. Griffond et G. Casalis. AIAA paper 2000-3806, 36th AIAA/ASME/SAE/ASEE Conf. Hunstville, Alabama, 16-19 Juillet 2000.

Motor Flow Instabilities - Part 2 : Intrinsic linear stability of the flow induced by wall injection. G. Casalis et F. Vuillot. RTO-AVT VKI Special Course on Internal Aerodynamics in Solid Rocket Propulsion. VKI Institut, 27-31 mai 2002. Conférencier invité.

Selection of acoustic modes in the vicinity of supersonic jets. Ch. Millet et G. Casalis. 8th AIAA/CEAS Aeroacoustics Conference, Breckenridge, USA, 17-19 juin 2002.

Particle effects on solid-propellant motors flow stability. Th. Feraille, G. Casalis et J. Dupays. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, USA, 7 - 10 Juillet 2002.

Relationship between instability waves and noise of low supersonic jets. Ch. Millet et G. Casalis. 23rd Congress of ICAS, Toronto, Canada, 8 - 13 septembre 2002.

Global Stability of the Flow induced by wall injection. G. Casalis, F. Chedevergne, Th. Féraille et G. Avalon. IUTAM,Symposium on Laminar-Turbulent Transition. Bangalore, Inde, 13-17 décembre 2004.

Modal analysis of a subsonic hot jet LES with comparison to the linear stability analysis. F. Müller, F. Vuillot, G. Rahier et G. Casalis. 11th AIAA/CEAS Aeroacoustics Conference, May 23-25, Monterey California, 2005.

Thrust Oscillations in Reduced Scale Solid Rocket Motors, part II : A New Theoretical Approach. F. Chedevergne et G. Casalis. Congrès AIAA/ASME, Joint Propulsion Conference, Tucson, Arizona, U.S., 10-13 juillet 2005.

Hydrodynamic Instability of the Ideal Hybrid Rocket. E. M. Abu-Isrhaid, J. Majadalani et G. Casalis. Congrès AIAA/ASME, Joint Propulsion Conference, Tucson, Arizona, U.S., 10-13 juillet 2005.

Experimental and Numerical Investigation of the Near Field Pressure of a High Subsonic Hot Jet. F. Müller, F. Vuillot, G. Rahier, G. Casalis et E. Piot. 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), Cambridge, Massachusetts, 8-10 Mai 2006.

A comparative use of the PSE and LES approaches for jet noise predictions. E. Piot, G. Casalis et F. Müller. 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), Cambridge, Massachusetts, 8-10 Mai 2006.

Detailed Analysis of the Thrust Oscillations in Reduced Scale Solid Rocket Motors. F. Chedevergne et G. Casalis. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2006-4424, Sacramento, 9-12 Juillet, U.S. 2006.

Stability of the Taylor-Culick Profile with Headwall Injection and Particles Interaction. L. Bhatia, A. Ishraid, J. Majadalani et G. Casalis. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2006-4424, Sacramento, 9-12 Juillet, U.S. 2006.

Simulation of ac-electroosmotic flows for concentration of particles on biosensors. L. Tanguy, G. Casalis et L. Nicu. 2007 NSTI Nanotechnology conference and Trade Show, Mai 20-24, Santa Clara, Californie, U.S., 2007.

Direct numerical simulation of the crossflow instabilities induced by a periodic roughness array on a swept cylinder : receptivity and stability investigations. E. Piot, G. Casalis et M. Terracol. 37th AIAA Fluid Dynamic Conference and Exhibit, June 25-28, Miami, Floride, US, AIAA Paper 2007-3976, 2007.

DNS Investigation of the Taylor-Culick Flow Stability Analysis. F. Chedevergne, G. Casalis and J. Majdalani. 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 8-11 July 2007, Cincinnati, Ohio.

Bi-global Linear Stability Analysis. G. Casalis, E. Piot, F. Chedevergne. 6th SIG33 workshop Laminar-Turbulent Transition Mechanisms, Prediction and Control, Kleinwalsertal, Austria, June 17-20, published in ERCOFTAC Bulletin, n. 74, september 2007.

Receptivity of the crossflow instabilities to a periodic roughness array on a swept cylinder : investigation of the roughness size influence. E. Piot, C. Content, G. Casalis. AIAA, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, 8-11 janvier 2008.

Laminar-turbulent transition control on a swept wing by micron-sized roughness elements. D. Arnal, G. Casalis, E. Piot. Congrès AAAF, "Maîtrise de la traînée et des nuisances", Poitiers, 10-12 mars, 2008.

DNS investigation of the flow induced by an unsteady wall injection. G. Casalis, F. Chedevergne. Space Propulsion 2008, Héraklion, Crète, 5-9 mai, 2008.

Global instability of an inviscid compressible flow over a cavity. F. Méry, G. Casalis. Sixth Internation Conference of Numerical Analysis and Applied Mathematics, Kos, Grèce, 16-20 septembre, 2008.

Automatic Transition Predictions using Simplified Methods. J. Perraud, D. Arnal, G. Casalis, J.-P. Archambaud, R. Donelli. 47th AIAA Aerospace Sciences Meeting, Orlando, Floride, U.S.A., 5-8 janvier, 2009.

Noise Generation Analysis of a Cylindrical Cavity by LES and Global Stability. F. Méry, D. Mincu, G. Casalis, A. Sengisson. 15th AIAA/CEAS Aeroacoustics Conference, Miami, Florida, U.S.A., May 11-13, 2009.

DNS Investigations of steady receptivity mechanisms on a swept cylinder. G. Casalis, E. Piot. Seventh IUTAM Symposium on Laminar-Turbulent Transition, June 23-26, Stockholm, Sweden, 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. Sapce Propulsion, 3-6 May, San Sebastian, Spain, 2010.

Simulation of a solid propellant subscale motor with a 3D protruding inhibitor. E. Radenac, G. Casalis, Y. Fabignon, M. Prévost. Sapce Propulsion, 3-6 May, San Sebastian, Spain, 2010.

Innovative tool for realistic cavity flow analysis : global stability. F. Méry, G. Casalis. The sixth international conference on computational fluid dynamics. St Pétersbourg, Russie, 12-16 juillet 2010.

Some recent advances in the instabilities occuring in long Solid Rocket Motors. G. Casalis, G. Boyer, E. Radenac. 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. 31 juillet - 3 août, San Diego, USA, 2011.

Theoretical and numerical investigation of optimal impedance in lined ducts with flow. J. Rodriguez Sanchez, E. Piot, G. Casalis. Acoustics, 23-27 avril, Nantes, 2012.

On the development and successful application of a thrust modulation module for the FUSEX hybrid rocket motor. J. Hijlkema, G. Casalis, F. Laurendeau. Space Propulsion, 7-10 mai, Bordeaux, 2012.

Discontinuous Galerkin method for acoustic modes computation in lined ducts. L. Pascal, E. Piot, G. Casalis. 18th AIAA/CEAS Aerouacoustics Conference. 4-6 juin, Colorado Springs, USA, 2012.

Theoretical investigation of the parietal vortex shedding in solid rocket motors. G. Boyer, G. Casalis, J.L. Estivalèzes. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Atlanta, Georgia, USA, 2012.

Laminar-Turbulent Transition Investigation in a Solid Rocket Motor Representative Cold Flow Setup. B. Gazanion, F. Chedevergne, X. de Saint Victor, J.-L. Estivalèzes, G. Casalis. AIAA-2013-3918, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit : Solid Rocket Propulsion.

Reduction of SRM Pressure Oscillations Through the Use of Fuel Grains with different Burn Velocities. J. Anthoine, P. Jézéquel, P. Prévot, M. Prévost et G. Casalis. AIAA-2013-4022, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit : Solid Rocket Propulsion, 2013.

Analyse de stabilité globale et instabilité hydrodynamique dans un conduit traité acoustiquement. L Pascal, E. Piot et G. Casalis. CFA 2014, 22-25 avril, Poitiers, France, 2014.

URANS Simulations of injection-driven flows with an imposed transition model. B. Gazanion, F. Chedevergne et G. Casalis. Space Propulsion 2014, 19-22 mai, Cologne, Allemagne, 2014.

Overview of transition prediction tools in the elsA software. J. Perraud, H. Deniau, G. Casalis. 11th World Congress on Computational Mechanics, 20-25 July, Barcelona, Spain, 2014.

Optimal disturbance in a flow duc with a lined wall. L. Pascal, E. Piot, G. Casalis. IUTAM_ABCM Symposium on Laminar Turbulent Transition, 8-12 Septembre, Rio de Janeiro, Brésil, 2014.

Experimental and numerical study of boundary layer transition control over an airfoil using a DBD plasma actuator. N. Szulga, O. Vermeersch, M. Forte, G. Casalis. IUTAM_ABCM Symposium on Laminar Turbulent Transition, 8-12 Septembre, Rio de Janeiro, Brésil, 2014.

Experimental and numerical study of the effect of gaps on laminar turbulent transition of incompressible boundary layers. M. Forte, J. Perraud, A. Séraudie, S. Béguet, L. Gentili, G. Casalis. IUTAM_ABCM Symposium on Laminar Turbulent Transition, 8-12 Septembre, Rio de Janeiro, Brésil, 2014.

Large Eddy Simulation of the Laminar-Turbulent Transition in the Flow induced by Wall Injection. B. Gazanion, F. Chedevergne, G. Casalis. IUTAM_ABCM Symposium on Laminar Turbulent Transition, 8-12 Septembre, Rio de Janeiro, Brésil, 2014.

Experimental and numerical study of the effect of gaps on the laminar-turbulent transition of two-dimensional incompressible boundary layers. M. Forte, L. Gentili, S. Béguet, J. Perraud et G. Casalis. 50th International Conference on Applied Aerodynamics - AERO 2015, 3AF AERO 2015, Toulouse, France, 30 Mars - 01 Avril, 2015.

Stabilizing boundary layers using a DBD plasma actuator : experimental and numerical study of the mean body force effect. N. Szulga, O. Vermeersch, M. Forte et G. Casalis. 50th International Conference on Applied Aerodynamics - AERO 2015, 3AF AERO 2015, Toulouse, France, 30 Mars - 01 Avril, 2015.

Experimental characterization of a Plasma Synthetic Jet. François Laurendeau, Olivier Léon, François Chedevergne et Grégoire Casalis. 50th International Conference on Applied Aerodynamics - AERO 2015, 3AF AERO 2015, Toulouse, France, 30 Mars - 01 Avril, 2015.

A survey of recent activities in transition modelling at Onera. G. Casalis. 11th ERCOFTAC SIG 33 Workshop, Progress in Transition Modelling and Control, St Helier, Jersey, UK, April, 15-17, 2015

PIV and Electric Charaterization of a Plasma Synthetic Jet Actuator. François Laurendeau, Olivier Léon, François Chedevergne et Grégoire Casalis. AIAA AVIATION 2015 - 45th AIAA Fluid Dynamics Conference -Dallas-U.S.A, 22-26 Juin, 2015.

Nonlinear interaction analysis of subsonic jet instabilities with forced eigenmodes using PSE. Maxime Itasse, Jean-Philippe Brazier et Grégoire Casalis. 21st AIAA/CEAS Aeroacoustics Conference, Dallas, U.S.A, 22-26 Juin 2015.

Influence of a 15° inclined nozzle on pressure oscillations in sub-scale solid rocket motors. J. Anthoine, L. Parassouramin-Vally, M. Prévost, N. Lupoglzoff, Y. Fabignon, G. Casalis, S. Larrieu, F. Godfroy, N. Cesco, Ph. Supié. 6th European Conference for Aeronautics and Space Sciences EUCASS 2015 - Cracovie, Pologne, 29 Juin-03 Juillet, 2015.

Stabilizing a Blasius Boundary Layer with Dielectric Barrier Discharge Plasma Actuation : Experimental Characterization and Numerical Modeling. Natacha Szulga, Olivier Vermeersch, Maxime Forte et Grégoire Casalis. 6th European Conference for Aeronautics and Space Sciences EUCASS 2015 - Cracovie, Pologne, 29 Juin-03 Juillet, 2015.

Database approach for 2D flow transition prediction in a RANS code. Bégou G., Deniau H., Vermeersch O., Casalis G. AIAA June 2016.