Absolutely, I can help you with running CFX coupled transient structural analysis on Linux without a GPU.
Visualization on Linux for Transient Structures:
Quick Tips and Tricks, Tutorials for Ansys , OpenFoam , OpenSource FEA and more
Absolutely, I can help you with running CFX coupled transient structural analysis on Linux without a GPU.
Visualization on Linux for Transient Structures:
Entering a small thickness like 1.5 mm into a large domain in ANSYS Fluent can be challenging due to meshing limitations and potential contact issues. Here are some approaches to consider:
Unfortunately, ANSYS Fluent doesn't offer a direct way to modify the number format for DPM (Discrete Phase Model) sample output. The output format is typically fixed in scientific notation (e.g., 1.1e+00).
Here are some alternative approaches you can consider:
Here's a breakdown to solve beam vibration problem of the general process after obtaining the equations from your free body diagram:
The DTRM model likely focuses on illumination parameters relevant for visible light rather than the entire solar radiation spectrum. Here's how to provide a more comprehensive input model for solar radiation in Ansys Fluent:
It sounds like you're encountering an unphysical increase in velocity for your bubble as it reaches the surface in your VOF-DPM coupled simulation. Here are some potential causes and solutions to consider:👽👿
Several factors can influence the presence or absence of a gas layer at the bottom of buried tubes in a Eulerian two-fluid fluidized bed simulation:
In multicomponent flow simulations without reactions, the exact value of the molar mass for each component doesn't significantly affect the mass fraction results in ANSYS CFX. Here's why:
Here's how to address your questions about plotting pressure change and determining pressure drop in ANSYS Fluent:
Plotting Pressure Change:
* Surface Reports: Utilize Surface Reports in ANSYS Fluent to obtain average pressure values at the inlet and outlet faces.
Iso-surface movement during SLM simulation in ANSYS can be caused by several factors. Here are some potential causes and solutions to consider:
👽
* Inaccurate Melt Pool Dynamics: The melting behavior of the powder might be misrepresented in your simulation. Calibrate your material properties, laser power settings, and melt pool viscosity to better reflect reality.
* Meshing Issues: A coarse mesh might not capture the melt pool dynamics accurately. Refine your mesh, particularly around the laser-powder interaction zone, to improve precision.
There are two possible reasons why you might not be able to see the vorticity contours in ANSYS CFD-Post:
The unexpected velocity increase in your partially filled stirred vessel simulation could stem from a few factors:
Hey everyone,
I have a weird problem with my simulation of a stirred vessel partially filled with water. Above the air-water interface, the velocity of water (UWater) gradually increases over time and I can't figure out why. I think this increase over time causes my simulation to fail after simulating a few seconds
I mostly used the case from this link as a reference: https://www.cemf.ir/simulating-two-p...sing-openfoam/
I can't figure out what the problem is for the increase. Does anyone know what could be the cause for this or had similar issues in the past?
There are two main approaches to porting the initial field from a StarCCM+ simulation to an OpenFOAM case:
* Using ccmToFoam: While ccmToFoam can convert the mesh, it may not directly translate the initial field data. You'll need to manipulate the converted data to match OpenFOAM's format.
In OpenFOAM, you can simulate rough wall effects in your pipe flow simulations using the roughWall function object. This function alters the logarithmic law of the wall to account for the increased drag caused by the roughness.
To access the raw GeoJSON string within a nested part of your server response without decoding the entire structure, you can use the decodeIfPresent(_:forKey:) method of the Decoder object. Here's how you can modify your code:
I am trying to install the OpenFOAM 11 version of thew software on my Windows server 22 OS through WSL. I followed the documentation based on the 4 steps mentioned here.
https://openfoam.org/download/source...g-environment/
While sourcing the bashrc file through my $HOME directory, I am getting the following errors as shown in the image attached. Do I need to make any changes in the User editable portion of the bashrc script?
To help with the 'mover' in OpenFOAM 11, specifically the 'interpolator' option.
While there seems to be a lack of readily available examples or tutorials on the 'interpolator' option in OpenFOAM 11's 'mover' dictionary, here's some insight that might be helpful:
The error message "Try signing in with a different account" usually indicates an issue with the Google account being used for login. Here are some troubleshooting steps you can try:
ClosedXML is a good choice for working with Excel files in C#. Here's a refined approach to achieve your goal:
* Read Error Code: Prompt the user to enter the error code using textBox1.Text.
The issue you're facing with the text appearing as ??? in the generated JPG file when executing the EXE from your ASP.NET application could be due to several reasons:
* Encoding Mismatch: The encoding used by your ASP.NET application might differ from the encoding expected by the external EXE. Try specifying the encoding for the command line arguments using Encoding.UTF8.GetBytes().
Backflow in OpenFOAM simulations can arise from various factors, even when using the inletOutlet boundary condition. Here are some potential causes and solutions for your specific scenario:
There is the inconsistency in units for non-Newtonian viscosity calculations in the Herschel-Bulkley model. The inconsistency arises because the model expresses shear stress (tau) in units of N/m^2 (Pascals), while the shear rate (gamma_dot) is in units of s^-1 (reciprocal seconds).
Setting up a simulation for 2D homogeneous isotropic turbulence (HIT) in Ansys Fluent requires defining a specific flow condition. While Fluent itself may not have a pre-configured template for HIT, you can achieve this by following these steps:
The error message you're encountering in Ansys Electronics Desktop
The quality of some mesh elements is not acceptable for solution. Please check the geometry for issues in the following location..
indicates that the mesh quality in a specific location (X=0.00536424, Y=-0.0146285, Z=-0.0061444) is below the acceptable threshold for accurate simulation results. Here are some steps you can take to address this issue:
The error message "Carrier phase curlUc interpolation object not set" in OpenFOAM indicates that a required interpolation object for the Saffman Mei lift force calculation is missing. Here's how to address this:
Converting rheology data to model parameters is definitely possible! Here's a general approach for fitting your complex rheology data (G*, G', and G'') to the PTT or Maxwell models using OpenFOAM:
DesignFOIL allows exporting airfoil coordinates in various formats, including DAT files. However, AirfoilTools specifically requires a DAT file format with a header containing specific information about the airfoil.
Here are some suggestions for your simulation of melting a phase change material (PCM) in an open cup:
Boundary Condition at Top (1):
The small gap you're encountering when extracting the internal volume in your pressure tank model with tubes is likely due to slight geometric imperfections or tolerances between the separate parts in your CAD software. Here are a few approaches you can try to fix this:
Yes, you can likely use the Transition SST model for your Darrieus turbine simulation in ANSYS FLUENT given the y+ wall value of approximately 1. Here's why:
I'd be glad to help you with the dynamic library error you're encountering in your OpenFOAM simulation. While I cannot provide specific instructions on copying and pasting due to the potential variations in file structures and operating systems, here are general guidelines that should help you resolve the issue:
The error message indicates that Abaqus is unable to locate a compatible C++ compiler on your system. Here are some potential solutions that you can try:
* Load vcvars64.bat: As suggested in the message, try loading the vcvars64.bat file before running Abaqus. This batch file sets up the environment variables for the Visual Studio C++ compiler. You can typically find it in the following location:
C:\Program Files (x86)\Microsoft Visual Studio\2019\Community\VC\Auxiliary\Build\vcvars64.bat
The error message "Not enough constraints applied to prevent rigid body motion" in Ansys Mechanical indicates that your PMSM rotor model is missing essential constraints to prevent it from undergoing unrealistic movements during the simulation. Here are some troubleshooting steps to address this:
In harmonic response analysis, applying a constant speed like in static structural analysis isn't possible because harmonic analysis focuses on the response of a system to varying excitation forces over a range of frequencies.
The timeVaryingMappedFixedValue boundary condition in OpenFOAM allows you to prescribe values that vary in time and space on a patch. Here's a breakdown of its usage with the interFoam solver:
The "Divergence detected in AMG solver" error in ANSYS Fluent indicates that the Algebraic Multigrid (AMG) solver is struggling to converge. This can arise from several factors, including:
Choosing the right solver in ANSYS Fluent depends on the nature of your fluid flow simulation:
Pressure-Based Solver:
* Ideal for incompressible flows (constant density) or low Mach number flows (below 0.3).
Calculating the Oscillatory Shear Index (OSI), Ig factor, Area Averaged Wall Shear Stress (AAWSS), and Time Averaged Wall Shear Stress (TAWSS) in ANSYS Fluent involves several steps. Here's a general guide to help you with the process:
ANSYS Mechanical renumbering cell zones/walls after mesh refinement is a common issue when dealing with journal files. Here are two approaches to address this:
In ANSYS Fluent, an opening boundary condition, also referred to as a pressure outlet boundary condition, is used to simulate an outlet where the flow exits the computational domain. It allows the fluid to leave the domain freely without any restrictions. Here's how to define it:
I have simulated unsteady fluidized bed at different superficial velocities and got result. now i want to plot a graph of expansion of bed vs superficial velocity. does fluent contain any option (xy plot) ?
The error message "Colour variable 'Velocity Meridional' does not exist" in ANSYS CFX indicates that the report template you're using is trying to reference a variable that doesn't exist in your simulation data. Here are a few ways to fix this issue:
You're right, in compressible boundary layers, increasing the Prandtl number (Pr) generally leads to a decrease in shear stress (skin friction) and Stanton number. Here's why:
Prandtl Number (Pr):
Pr is the ratio of momentum diffusivity (ν) to thermal diffusivity (α). It represents the relative ease with which momentum and heat diffuse within a fluid.
Ansys is a powerful commercial software suite, so there isn't a single free program that offers all its functionalities. However, depending on your specific needs, here are some free and open-source options that can handle various aspects of structural analysis similar to Ansys:
General Structural Analysis:
Both Ansys Discovery and Ansys SpaceClaim are Ansys software products, but they serve different purposes. Here's a breakdown of their pros and cons to help you decide which one is better for your needs:
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Choosing between a Sliding Mesh and MRF (Multiple Reference Frame) in ANSYS Fluent depends on the complexity of your simulation and the accuracy you require.
Imagine you're a detective trying to track down a mischievous gas bubble hiding in a swirling liquid. In the world of computational fluid dynamics (CFD), that bubble is your friend, and you're the CFD model trying to predict its movement.
Fluid mechanics with numerical analysis, also known as Computational Fluid Dynamics (CFD), is a powerful field! Here's a roadmap to get you started:
Ansys offers functionalities to model crack propagation through the Ansys Mechanical software and the SMART Crack Growth feature. Here's a general breakdown of the process:
1. Pre-Processing: