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Binary collision of CMAS droplets—Part I Equal-sized droplets Authors. Himakar Ganti Prashant Khare Luis Bravo Content type OriginalPaper Published 01 September 2020 Pages Binary collision of CMAS droplets—Part II Unequal-sized droplets Authors. Himakar Ganti High-energy X-ray phase analysis of CMAS-infiltrated

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The paper presents results from a numerical investigation of the non-central binary collision of two equal size droplets in a gaseous phase. The flow field is two phase and three dimensional the investigation is based on the finite volume numerical solution of the Navier–Stokes equations coupled with the Volume of Fluid Method (VOF

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Binary collision of CMAS droplets—Part II Unequal-sized droplets Himakar Ganti1 Prashant Khare1 a) Luis Bravo2 1Department of Aerospace Engineering University of Cincinnati Cincinnati OH USA 2Vehicle Technology Directorate Army Research Laboratory Aberdeen Proving Ground MD 21005 USA a)Address all correspondence to this author. e-mail prashant.khare uc.edu

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An extensive experimental investigation of the binary collision dynamics of water drops for size ratios of 1 0.75 and 0.5 for the Weber-number range of 1 to 100 and for all impact parameters is reported. Two different types of separating collisions namely reflexive and stretching separations are identified. Reflexive separation is

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Mar 01 2012 · Binary droplet collision is a phenomenon occurring in many engineering applications as in the binary collision between equal or unequal sized fuel droplets in fuel sprays inside internal combustion engines (ICE) ink-jet printing or in raindrop formation.

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The ChapmanEnskog equation is given by-732TM M 12 DAB = 1 858.(//) m 2 /s (2.54)Ps2 AB WD Here T = absolute temperature in K M A M B = molecular weights of the components A and B P = total pressure in atm s AB = a characteristic length parameter of the binary in W D = collision integral which is a function of kT/e AB (where k is the

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"Dynamics and Mass Transfer of Unequal-sized Droplet Collision " by X. D. Chen D. J. Ma and V. Yang AIAA Paper presented at 50th Aerospace Sciences Meeting and Exhibit January 2012. "Impinging Jet Dynamics and Atomization " by X. D. Chen D. J. Ma and V. Yang AIAA Paper presented at 50th Aerospace Sciences Meeting and

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A Three-Dimensional SPH Approach for Modelling the Collision Process Between Liquid Drops The Formation of Clusters of Unequal-Sized Drops . Part II Drops Particles and Waves Part III Multiphase and Multicomponent Flows Part IV Atmospheric and Granular Flows and Part V Turbulent and Astrophysical Flows.

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