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Questions and Answers

What is the primary goal of performing a mesh independence study?

  • To ensure the solution does not change with mesh refinement (correct)
  • To increase the complexity of the model
  • To validate the boundary conditions used
  • To reduce the computational time
  • What action should be taken if the monitor point values from Step 2 do not match the values from Step 1 within the allowable tolerance?

  • Change the solver settings
  • Proceed to refine the mesh further (correct)
  • Accept the results as valid
  • Adjust the boundary conditions
  • If monitor point values match within 5% in a mesh study, what does it indicate?

  • The mesh is too coarse for the analysis
  • The results are adequate for further analysis (correct)
  • The boundary conditions need reviewing
  • The simulation is complete and accurate
  • Why is it preferred to use three levels of mesh during a convergence study?

    <p>To ensure sufficient variation in results</p> Signup and view all the answers

    How does the accuracy of the mesh and boundary conditions affect the 'converged' solution?

    <p>Accuracy directly improves the reliability of the solution</p> Signup and view all the answers

    Which of the following best describes 'convergence' in computational fluid dynamics?

    <p>A state where the solution approaches a stable value</p> Signup and view all the answers

    What is the significance of defining correct boundary conditions in CFD modeling?

    <p>They are necessary for establishing physical constraints</p> Signup and view all the answers

    What does a significant difference in mass flow rate at inlets and outlets generally indicate?

    <p>Potential numerical instability or errors</p> Signup and view all the answers

    Which method captures large eddies directly and is more accurate than RANS?

    <p>Large Eddies Simulation (LES)</p> Signup and view all the answers

    In a compressible flow scenario, what is the pressure value represented by P?

    <p>101325 Pa</p> Signup and view all the answers

    Which boundary condition can be changed after mesh generation?

    <p>Pressure Inlet</p> Signup and view all the answers

    What does symmetry plane in CFD allow for?

    <p>Both geometry and flow symmetry</p> Signup and view all the answers

    Which of the following is NOT a guideline for specifying well-posed boundary conditions?

    <p>Keep conditions dependent on mesh refinement</p> Signup and view all the answers

    What type of boundary condition is often used to set a defined velocity inlet?

    <p>Velocity Inlet</p> Signup and view all the answers

    What is the primary purpose of performing a Mesh Independence Study?

    <p>To find the optimal mesh size that affects simulation results</p> Signup and view all the answers

    Which condition must be carefully defined to ensure accurate simulation in CFD?

    <p>Well-posed boundary conditions</p> Signup and view all the answers

    What describes periodic boundary conditions in CFD?

    <p>They are fixed and cannot change post-mesh generation.</p> Signup and view all the answers

    What is necessary for creating profile boundary conditions from experimental data?

    <p>An appropriately formatted file</p> Signup and view all the answers

    Study Notes

    CFD Setting Up Physics

    • This module covers computer-aided design and engineering (REE470) in Fall 2024.
    • Computational fluid dynamics (CFD) is used in the process.
    • Inlet and outlet conditions are visualized.
    • Velocity, pressure, and other related parameters are monitored.

    Lecture Outline

    • Recall of convergence, mesh independence, and validation methods.
    • Introduction to material properties.
    • Cell zone conditions are defined.
    • Boundary conditions are explained.
    • Mesh interfaces are discussed.
    • A summary of the lecture is presented.

    Convergence, Mesh Independence Study and Validation

    • The precision of the numerical solution relies on accurate mesh and boundary conditions.
    • Steady-state simulation should satisfy three conditions:
      • Residual RMS error values below 10⁻⁴ or 10⁻⁵.
      • Monitor points for values of interest reaching a steady state.
      • Imbalances in the domain less than 1%.
    • Expected patterns or phenomena (e.g., separation bubble, vortex shedding) in the flow field should also be exhibited.

    Convergence, Mesh Independence Study and Validation (Examples)

    • Graphs of monitoring residuals illustrate convergence trends.
    • Graphs show monitoring a value of interest, demonstrating a steady-state solution.
    • Monitoring domain imbalances demonstrates stability.
    • Critical values for the study are Residual RMS Error, Monitor points, and Domain imbalance.

    Convergence, Mesh Independence Study and Validation (Further Details)

    • Values of interest include pressure drop, forces, and mass flow rates.
    • These values should converge to a steady state.
    • Residual RMS Error values should be at least 10⁻⁴.
    • Domain imbalance should be less than 1%.

    Convergence, Mesh Independence Study and Validation (Mesh Independence Study)

    • A single solution is generated for the given mesh.
    • Next, mesh independence is ensured via refinements to the mesh.
    • Monitoring points from Step 2 are compared with those from Step 1, ensuring consistency within tolerance (e.g., 5%).
    • If values differ, refining the mesh and repeating the process is required.
    • Three levels of mesh are generally preferred.

    Convergence, Mesh Independence Study and Validation (Step 3)

    • If the solution changes with refinement, a mesh-independent solution hasn't been achieved.
    • Refinement and repetition are required until a mesh-independent solution is reached. Use the smallest possible mesh size to reduce simulation time.

    Convergence, Mesh Independence Study and Validation (Example)

    • Monitor values are plotted against the number of cells.
    • Differences in calculated values with increasing mesh resolution can be identified, and a mesh-independent result using the smallest mesh size is presented.

    Convergence, Mesh Independence Study and Validation (Further Discussion)

    • Analysis of global values like average temperature at the outlet for accurate results and further analysis, and use of 6 million cells.
    • Comparison of profiles at specific points (e.g., velocity or temperature.).
    • Tables can be used to compare different levels of mesh with respect to their accuracy.

    Validation with Experimental Measurements

    • Validation is the process of determining a model's accuracy in representing the real world.
    • Analytical solutions, experimental measurements, or literature computations from similar studies can be used for validation.
    • Large eddies are critical for momentum transfer and turbulent mixing in fluids.
    • The RANS approach models these.

    Introduction

    • Defining material properties, cell zones, and boundary conditions, using Fluent, is crucial.
    • Accuracy of simulations relies on properly defining these aspects.
    • Learning aims include defining material properties, boundary condition types, defining mesh interfaces and cell zones.

    ANSYS Fluent Workflow

    • This covers steps in setting up, simulating, and post-processing in ANSYS Fluent.
    • Domain setting, physics setup, solving, and post-processing are described.
    • Instructions will match the arrangement in COMSOL.

    Setting Up Physics: Other Group Boxes

    • There's no need to change solver settings unless a simulation is transient or involves high-speed compressible flow.
    • Commonly used models include energy, heat transfer, radiation, viscous turbulence, multiphase, species, and discrete phase models.

    Setting Up Physics: Create/Edit Materials

    • Fluent offers a database of predefined fluids, solids, and mixtures.
    • User-defined materials, accessed and modified via the standard materials panel, can be created.

    Fluid Density

    • In incompressible flows, density is constant.
    • Ideal gas properties require specifying density as a function of temperature.
    • Polynomial functions or laws for compressible flows are used to define density as a function of pressure and temperature.

    Operating Pressure

    • Operating pressure is an absolute pressure datum with other relative pressures measured from it.
    • It is used to avoid round-off errors in simulations where dynamic pressure differences are small compared to the absolute pressure.

    Cell Zones and Boundary Zones

    • Cells in a mesh are grouped into zones.
    • Each cell is bounded by faces that form face zones.
    • Some of these faces form boundary zones, those faces on the boundaries of the model.

    Setting Up Physics: Cell Zones

    • Cell zones help assign materials to different regions (fluid, solid, porous, etc.) of the domain.
    • Cell zone conditions are defined to specify properties for different cells.

    Setting Up Physics: Cell Zones (Additional)

    • A cell zone is a group of cells for which all active equations are solved.
    • A fluid cell zone can be more simply understood as a group of cells for which all fluid equations are solved.
    • A solid zone is a group of cells for which only the heat conduction equation is solved, flow equations are not solved.

    Setting Up Physics: Boundaries

    • Boundaries are defined and filtered by type (inlets, outlets, walls, etc.)
    • Boundary types are pre-defined in the preprocessing phase.
    • Boundary conditions can be changed after mesh generation for most, except for periodic BCs.

    Defining Boundary Conditions

    • Boundary conditions define dependent variables on domain boundaries.
    • Examples include mass, momentum, and energy fluxes.
    • Critical factors for boundary conditions include geometry, location, available data, and model constraints.

    Available Boundary Condition Types

    • External boundaries encompass different flow scenarios (pressure inlet, pressure outlet, velocity inlet, and outflow).
    • Internal boundaries define components (fans, interior, porous jump, radiators, walls).

    General Guidelines for Boundaries in CFD

    • Flow direction at inflow/outflow boundaries should ideally be normal to the boundary.
    • Large gradients normal to boundaries should be avoided if possible.
    • Minimize grid skewness for accuracy of simulations.

    Symmetry Planes

    • Symmetry planes have zero normal velocity and zero normal gradients.
    • No explicit inputs are required.
    • The geometry and flow must be symmetric around the plane.

    Specifying Well Posed Boundary Conditions

    • Boundaries near recirculation zones should be placed downstream to allow the correct flow development.
    • Location choices have effects on turbulence, temperature, and species-related boundary conditions.

    Specifying Well Posed Boundary Conditions (Inlet/Outlet)

    • Combination of velocity inlet and static pressure outlet is generally most robust, mass flow in and static pressure out are robust.
    • For total and static pressure inlet with outflow, the combination is sensitive to initial guesses.
    • Avoid using total pressure inlet with outflow type.

    Specifying Well Posed Boundary Conditions

    • Boundaries near recirculation zones should be placed downstream.
    • Boundaries must be selected carefully for accurate results.

    Specifying Well Posed Boundary Conditions (Domain Size)

    • Computational domain should be large enough for accurate solutions, especially with high pressure gradients, where pressure gradients are large, the domain needs to be large.

    Defining Boundary Conditions (Further Discussion)

    • Boundary conditions affect the behavior of the solution, especially with convergence.
    • Accurate choices depend on geometry and available data.

    Periodic Boundary Condition

    • Simplifies the simulation by reducing overall mesh size.
    • Periodic conditions can be translational or rotational for specific geometries.

    Summary

    • Cell zones assign materials.
    • Fluent has a material database.
    • Boundary zones define BCs at internal/external boundaries, and mesh interfaces.
    • Convergence and accurate results depend on correct boundaries.

    Appendix (Tips & Tricks)

    • Skewness is defined using angle deviation and relates to cell quality.
    • Normalized skewness values help evaluate cell quality.
    • Optimal cell size and cell quality are relevant to the mesh.

    Appendix: Options for Defining Common Properties

    • Options for defining density, thermal conductivity, viscosity, and specific heat are presented.
    • These properties are defined as constant, dependent on temperature, through kinetic theory, and user-defined.

    Case Setup Replication

    • Use TUI commands or the file interface for case setup replication to transfer settings from a 2D case to a 3D case by changing the mesh.

    Cell Zone Definition - Fluid

    • Selecting a fluid material is crucial in defining the fluid zone contents.
    • This is essential for multiple species or multiphase flows.

    Cell Zone Definition - Solid

    • Identifying the solid material is the essential requirement.
    • Volumetric heat source rate can be defined.

    Profile Data and Solution Data Interpolation

    • Fluent allows interpolation of variable data at face and cell zones using profile and interpolation files.
    • Profile files contain point data for different variables on zones.
    • Interpolation files hold discrete data for variables on cell zones.

    Profile Boundary Conditions (e.g. Velocity Inlet)

    • Boundary conditions are applied in panels.
    • Profiles are selected for input to the boundary conditions.
    • Details on these conditions are in the user guide.

    Boundary Zone: Velocity Inlet

    • Velocity inlet is suited for incompressible flows, but not recommended for compressible flows, and uses UDFs, magnitudes and direction for input.

    Boundary Zone: Pressure Inlet

    • Pressure inlets allow static pressure or total pressure input.
    • Pressure inlet is suitable for both compressible and incompressible flows.
    • Turbulence data and total temperature are crucial for the correct treatment.

    Boundary Zone: Mass Flow Inlet

    • Mass flow inlets define total mass flow rate or mass flux.
    • Suitable for both compressible and incompressible flows.
    • Difficult to converge.

    Boundary Zone: Pressure Outlet

    • Outlet conditions are important for specifying the flow's exit with gauge pressure.
    • Backflow information can be important and helpful for inlet and outlet definitions.

    Boundary Zone: Outflow

    • Outflow boundaries don't need pressure or velocity input but are appropriate only for fully defined exits.
    • This boundary is unsuitable for unsteady flows with variable density or backflow.

    Modelling Multiple Exits

    • Pressure outlet or outflow boundaries can be assigned to model flows with multiple exits.
    • Mass flow rate fraction from Flow Rate Weighting, varies from 0 to 1.

    Boundary Zone: Wall

    • No-slip conditions are applied at walls in viscous flows.
    • Wall roughness can be defined for turbulent flows.

    Axis Boundaries

    • Axis boundaries are assigned at the center line for axi-symmetric 2D problems and are not used for 3D cases.

    Other Inlet/Outlet Boundary Conditions

    • Pressure far field and exhaust fan/outlet vent are discussed.
    • Modeling for these specific elements using appropriate boundaries is described.

    Periodic Boundaries

    • Periodic boundaries are used to reduce mesh size and are based on rotational or translational periodicity.

    Internal Face Boundaries

    • Internal faces enable step changes in flow properties, crucial for implementing various physical models (fans, radiators, porous jump models).

    Specifying Well-Posed Boundary Conditions (Turbulence)

    • Turbulence intensity and viscosity ratio are crucial for specifying turbulence for complex flows.
    • Good estimates are useful for preliminary simulations.

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