By Thomas Doll
SB2U Vindicator in motion КНИГИ ;ВОЕННАЯ ИСТОРИЯ Издательство: Squadron/Signal publicationsСерия: airplane 122Язык: EnglishISBN: 0-89747-274-8Формат: pdfРазмер: 15.4 mbRapid eighty five
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Kinetic equation for particle transport and heat transfer in nonisothermal turbulent flows. AIAA Paper No. 2002-0337. 15. Pandya, R. V. , and F. Mashayek. 2002. Nonisothermal dispersed phase of particles in turbulent flow. J. Fluid Mechanics 475:205-45. 16. Miller, R. , K. Harstad, and J. Bellan. 1998. Evaluation of equilibrium and nonequilibrium evaporation models for many-droplet gas-liquid flow simulations. Int. J. Multiphase Flow 24:1025. 17. Mashayek, F. 1998. Droplet-turbulence interactions in low-Mach-number homogeneous shear two-phase flows.
In DNS of single-phase flows, a complete set of compressible Navier-Stokes, energy, and scalar transport equations are calculated together with the equation of state and some constitutive relations . In DNS of particle-laden flows, in addition to carrier-gas equations, the Lagrangian form of particle (droplet) equations are solved via "standard" diff'erence schemes . For LES of two-phase flows, the large-scale Eqs. 4) and the filtered energy equation are solved for the carrier-gas phase together with Mean Kinetic Energy Velocity (MKEV)  SGS stress and diff'usivity closures.
5. This figure shows the Speckle displacement field superposed to the temperature. The temperature is obtained by converting the refractive index values using the Gladstone-Dale law. The underlying assumption is that the behavior of the gas mixture can be well approximated by ideal gas. The temperature estimate is well within the expected range as the adiabatic flame temperature for a propaneair mixture flame is 1977 ^C. This is the maximum temperature that a propaneair flame can reach under atmospheric pressure and for <]^ = 1.