Modélisation de l'écoulement diphasique dans les injecteurs Diesel

BIBLIOGRAPHIE 167[92] R. MARCER. Simulation des écoulements d’injecteur diesel avec le code eole-projet 1998. Technicalreport, PRINCIPIA, 1998.[93] R. MARCER and J.M. LEGOUEZ. Simulation of unsteady cavitating fl ows in diesel injector withan improved vof method. In ILASS - Europe 2001, Zurich, CH, 2001.[94] K. MOKADDEM and P. LESSART. Base de données sur moteur transparent en injection directeDiesel common rail : visualisation des phases liquide et vapeur des jets. Technical Report 45337,Institut Français du Pétrole, 1999.[95] A. NISHIMURA and D.N. ASSANIS. A model for primary diesel fuel atomization based on cavitationbubble collapse energy. In Eight International Conference on Liquid Atomization and Spraysystems ICLASS2000, Pasadena, CA, USA, 2000.[96] W.F. NOH and P. WOODWARD. Slic : Simple line interface calculation. In Proc. Fifth Int. Conf.on Numerical Methods in Fluid Dynamics. Springer-Berlin.[97] W.H. NURICK. Orifice cavitation and its effect on spray mixing. J of Fluids Engineering, 98, 1976.[98] C.D. OHL, A. PHILIPP, and W. LAUTERBORN. Aufnahme des kollapsvorganges laserindurzierterkavitäten mit 20 millionen bildern pro sekunde. ?, 1997.[99] T.R. OHRN, D.W. SENSER, and A.H. LEFEBVRE. Geometric effects on spray cone angle forplain orifice atomizers. Atomization and Sprays, 1, 1991.[100] P.J. O’ROURKE and A.A. AMSDEN. The tab method for numerical calculation of spray dropletbreakup. SAE paper 872089, 1987.[101] S.V. PATANKAR. A calculation procedure for two-dimensional elliptic situations. Numerical HeatTransfer, 4 :409–425, 1981.[102] S.V. PATANKAR and D.B. SPALDING. A calculation procedure for heat, mass and momentumtransfer in three-dimensional parabolic fl ows. Int. J. Heat Mass Transfer, 15 :1787–1806, 1972.[103] M. PILCH and C.A. ERDMAN. Use of breakup time data and velocity history data to predict themaximum size of stable fragments for acceleration-induced breakup of a liquid drop. InternationalJournal of Multiphase Flow, 13(6) :741–757, 1987.[104] T. POINSOT and D. VEYNANTE. Theoretical and Numerical Combustion. R.T. Edwards, 1994.[105] T.J. POINSOT and S.K. LELE. Boundary conditions for direct simulations of compressible viscousfl ows. Journal of Computational Physics, (101) :104–129, 1991.[106] L.N. RANDALL. Rocket applications on the cavitating venturi. ARS Journal, 1952.[107] E. RAPPOSELLI and L. D’AGOSTINO. Numerical modeling of sheet and tip vortex cavitationwith fl uent 5. In A Modified Isenthalpic Model of Cavitation in Plane Journal Bearings, volumehttp ://cav2001.caltech.edu, Pasadena, CA, USA, 2001.[108] J.L. REBOUD, B. STUTZ, and O. COUTIER. Two-phase fl ow structure of cavitation : experimentand modelling of unsteady effects. In 3rd International Symposium on Cavitation, volume 1, pages203–208, 1998.[109] R.D. REITZ. Atomization and other beakup regimes of a liquid jet. PhD thesis, Princeton University,1978.[110] R.D. REITZ. Modeling atomization processes in high-pressure vaporizing sprays. Atomisation andSpray Technology, 3 :309–337, 1987.[111] R.D. REITZ and F.V. BRACCO. Mechanisms of breakup of round liquid jets. The encyclopedia offl uid mechanics, 3 :233–249, 1986.[112] A.J. RUIZ. A few useful relations for cavitating orifices. In ICLASS’91, 1991.[113] J.H. RUPE. On the dynamic characteristics of free-liquid jets and a partial correlation with orificegeometry. Technical Report 32, J.P.L., 1962.[114] D.P. SCHMIDT. The cavalry model. 1997.[115] D.P. SCHMIDT. Cavitation in Diesel fuel injector nozzles. PhD thesis, University of Wisconsin -Madison, 1997.