The expansion through the nozzle is so quick that condensation within the vapor does not occur (due to very small time). The vapor expand as superheated vapor until some point at which condensation occurs suddenly and irreversibly.
Key points: The expansion through the nozzle is so quick that condensation within the vapor does not occur (due to very small time). The vapor expand as superheated vapor until some point at which condensation occurs suddenly and irreversibly.
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Heat And Mass Transfer With The volume of fluid Model And Evaporation-Condensation ModelTo be added. Heat and mass transfer with the mixture model and evaporation-condensation modelTo be added. videosHeat and mass transfer between two phases (half liquid) using the Volume of Fluid (VOF) multi-phase model in ANSYS FLUENT along with Evaporation-Condensation model - Contours of volume of fluid Heat and mass transfer with the mixture model and evaporation-condensation model - Contours of static temperature (mixture) Heat and mass transfer with the mixture model and evaporation-condensation model - Contours of velocity magnitude (mixture) referenceTutorial: Using the Volume of Fluid (VOF) model
Introduction to User Defined Functions (UDF)
Examples of User Defined Functions (UDF)
Fluent User Defined Functions (UDF) manual
Tutorial: comparison of using the mixture and eulerian multiphase models
Horizontal film boiling simulation by Fluent
Good video of CFD nucleate boiling using FLUENT / ANSYS by M. Habte. Ph.D., Mechanical Engineering CFD Simulation of Pool Boiling Phenonmena by Yi Liu. Different boiling phenonmena including Film boiling, Transition boiling and Nucleate boiling are identified by CFD simulation. download
1. Nusselt number
average Nusselt number: Nu_L= convective heat transfer/conductive heat transfer = hL/k where L is the characteristic length, k is the thermal conductivity of the fluid, h is the convective heat transfer coefficient of the fluid. Selection of the characteristic length should be in the direction of growth (or thickness) of the boundary layer; some examples of characteristic length are: the outer diameter of a cylinder in (external) cross flow (perpendicular to the cylinder axis), the length of a vertical plate undergoing natural convection, or the diameter of a sphere. For complex shapes, the length may be defined as the volume of the fluid body divided by the surface area. The thermal conductivity of the fluid is typically (but not always) evaluated at the film temperature, which for engineering purposes may be calculated as the mean-average of the bulk fluid temperature and wall surface temperature. local Nusselt number: Nu_x = h_x*x/k The length x is defined to be the distance from the surface boundary to the local point of interest. 2. Prandtl number The Prandtl number Pr is a dimensionless number, named after the German physicist Ludwig Prandtl, defined as the ratio of momentum diffusivity (kinematic viscosity) to thermal diffusivity. That is, the Prandtl number is given as: Pr = viscous diffusion rate/thermal diffusion rate = nu/alpha = Cp*mu/k where: nu : kinematic viscosity, nu = mu/rho, (SI units : m²/s) alpha : thermal diffusivity, alpha = k/(rho*Cp), (SI units : m²/s) mu : dynamic viscosity, (SI units : Pa*s = N*s/m²) k: thermal conductivity, (SI units : W/(m*K) ) Cp : specific heat, (SI units : J/(kg*K) ) rho : density, (SI units : kg/m³ ). 3. Reynolds number The Reynolds number is defined as the ratio of inertial forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow conditions. The Reynolds number is defined below for each case. Re = inertial forces/viscous forces = rho*v*L/mu = v*L/nu where: v is the mean velocity of the object relative to the fluid (SI units: m/s) L is a characteristic linear dimension, (travelled length of the fluid; hydraulic diameter when dealing with river systems) (m) mu is the dynamic viscosity of the fluid (Pa·s or N·s/m² or kg/(m·s)) nu is the kinematic viscosity (nu = mu/rho) (m²/s) rho, is the density of the fluid (kg/m³). 4. Péclet number The Péclet number (Pe) is a dimensionless number relevant in the study of transport phenomena in fluid flows. It is defined to be the ratio of the rate of advection of a physical quantity by the flow to the rate of diffusion of the same quantity driven by an appropriate gradient. The Péclet number is defined as: Pe = advective transport rate/diffusive transport rate For diffusion of matter (mass diffusion), it is defined as: Pe_L = L*U/D = Re_L/Sc For diffusion of heat (thermal diffusion), the Péclet number is defined as: Pe_L = L*U/alpha = Re_L/Pr where L is the characteristic length, U the velocity, D the mass diffusion coefficient, and alpha the thermal diffusivity, alpha = k/(rho*Cp) where k is the thermal conductivity, rho the density, and Cp the heat capacity. 5. Stanton number The Stanton number, St, is a dimensionless number that measures the ratio of heat transferred into a fluid to the thermal capacity of fluid. It is used to characterize heat transfer in forced convection flows. St = h/G*Cp = h/(rho*u*Cp) where: h = convection heat transfer coefficient rho = density of the fluid Cp = specific heat of the fluid u = speed of the fluid It can also be represented in terms of the fluid's Nusselt, Reynolds, and Prandtl numbers: St = Nu/(Re*Pr) where: Nu is the Nusselt number; Re is the Reynolds number; Pr is the Prandtl number. 6. Mach number In fluid mechanics, Mach number (M or Ma) is a dimensionless quantity representing the ratio of speed of an object moving through a fluid and the local speed of sound. M = v_object/v_sound where: M is the Mach number, v_object is the velocity of the source relative to the medium, and v_sound is the speed of sound in the medium. 7. Schmidt number Schmidt number (Sc) is a dimensionless number defined as the ratio of momentum diffusivity (viscosity) and mass diffusivity, and is used to characterize fluid flows in which there are simultaneous momentum and mass diffusion convection processes. It is defined as: Sc = nu/D = mu/(rho*D) = viscous diffusion rate/molecular (mass) diffusion rate where: nu is the kinematic viscosity or (mu/rho) in units of (m²/s) D is the mass diffusivity (m²/s). mu is the dynamic viscosity of the fluid (Pa·s or N·s/m² or kg/m·s) rho is the density of the fluid (kg/m³). The heat transfer analog of the Schmidt number is the Prandtl number. 8. Biot number The Biot number (Bi) is a dimensionless quantity used in heat transfer calculations. It gives a simple index of the ratio of the heat transfer resistances inside of and at the surface of a body. The Biot number is defined as: Bi = h*Lc/k_b where: h = film coefficient or heat transfer coefficient or convective heat transfer coefficient Lc = characteristic length, which is commonly defined as the volume of the body divided by the surface area of the body, such that Lc = V_body/A_surface k_b = Thermal conductivity of the body 9. Rayleigh number In fluid mechanics, the Rayleigh number (Ra) for a fluid is a dimensionless number associated with buoyancy driven flow (also known as free convection or natural convection). When the Rayleigh number is below the critical value for that fluid, heat transfer is primarily in the form of conduction; when it exceeds the critical value, heat transfer is primarily in the form of convection. The Rayleigh number is defined as the product of the Grashof number, which describes the relationship between buoyancy and viscosity within a fluid, and the Prandtl number, which describes the relationship between momentum diffusivity and thermal diffusivity. Hence the Rayleigh number itself may also be viewed as the ratio of buoyancy and viscosity forces times the ratio of momentum and thermal diffusivities. For free convection near a vertical wall, the Rayleigh number is defined as Ra_x = g*β/(nu*α)*(Ts - T∞) x³ = Gr_x*Pr where: x = Characteristic length (in this case, the distance from the leading edge) Ra_x = Rayleigh number at position x Gr_x = Grashof number at position x Pr = Prandtl number g = acceleration due to gravity Ts = Surface temperature (temperature of the wall) T∞ = Quiescent temperature (fluid temperature far from the surface of the object) nu = Kinematic viscosity α = Thermal diffusivity β = Thermal expansion coefficient (equals to 1/T, for ideal gases, where T is absolute temperature) In the above, the fluid properties Pr, nu, α and β are evaluated at the film temperature, which is defined as Tf = (Ts + T∞)/2 For most engineering purposes, the Rayleigh number is large, somewhere around 10E6 to 10E8. For a uniform wall heating flux, the modified Rayleigh number is defined as Ra*_x = g*β*q''_o*x^4/(nu*α*k) where: q"_o = the uniform surface heat flux (W/m2) k = the thermal conductivity (W/m*K) 10. Grashof number The Grashof number (Gr) is a dimensionless number in fluid dynamics and heat transfer which approximates the ratio of the buoyancy to viscous force acting on a fluid. It frequently arises in the study of situations involving natural convection. Gr_L=gβ(Ts−T∞)L³/nu² for vertical flat plates Gr_D=gβ(Ts−T∞)D³/nu² for pipes Gr_D=gβ(Ts−T∞)D³/nu² for bluff bodies where the L and D subscripts indicate the length scale basis for the Grashof Number. g = acceleration due to Earth's gravity β = volumetric thermal expansion coefficient (equal to approximately 1/T, for ideal fluids, where T is absolute temperature) Ts = surface temperature T∞ = bulk temperature L = characteristic length D = diameter nu = kinematic viscosity The transition to turbulent flow occurs in the range 10E8<Gr_L<10E9 for natural convection from vertical flat plates. At higher Grashof numbers, the boundary layer is turbulent; at lower Grashof numbers, the boundary layer is laminar. The product of the Grashof number and the Prandtl number gives the Rayleigh number, a dimensionless number that characterizes convection problems in heat transfer. From Wikipedia: http://en.wikipedia.org/wiki/Category:Dimensionless_numbers_of_fluid_mechanics Ejectors for the oil and gas industry:
Ejectors for the nuclear industry:
The boundary layer form of the Navier-Stokes equations and their treatments
Ideal gas thermodynamic properties in Chemkin format
Simple equilibrium with multiple reactions
Convergence to most probable macrostate
Spectroscopy primer
Atomic spectroscopy (NIST)
Atomic spectra term symbol and Hunds rules
Atomic term symbols
Term symbol
Quantum mechanics and spectroscopy
Ideal diatomic gas (Table of molecular constants for several diatomic molecules included)
Burcat thermo data file
Courtesy to Professor Nick Glumac
Course website: http://glumac.mechse.illinois.edu/me404/INDEX.html Search engine optimization starter guide (English)
Search engine optimization starter guide (Chinese)
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Jingwei ZhuPh.D. candidate in the Department of Mechanical Science and Engineering at the University of Illinois at Urbana-Champaign. Categories
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