ANSYS Products 16.2 Win64 Design with ANSYS Products 16.2 Win64 full. The longer engineers wait for a working mesh, the less time they have to iterate, replace or fix their part based on the simulation results. Recently, Ansys Mechanical introduced the unstructured mesh method (UMM). This method will help engineers mesh their crack propagation simulation in minutes.
This method will help to speed up the development of stronger parts. Traditionally, simulating crack propagation means using hexahedral (hex) and wedge elements to capture the geometry of the crack and allowing the solver to run.
Ideally, the mesh would only involve hex elements and the solver would progress the crack through the mesh. The reality is that geometry is never that simple, and the crack’s path will not want to travel in the same direction as the mesh. Engineers can simplify the crack’s geometry until they can capture its behavior with only hex elements.
However, this leads to a loss of fidelity in the simulation. Alternatively, engineers can use UMM. The method reduces meshing time by automatically generating an all-tetrahedral (tet) mesh at the crack’s front.
is one of the leading software developers of CAE (Computer-Aided Engineering). This set includes various tools for simulation and analysis of various branches of engineering sciences such as electromagnetism, electrostatics, electronics, solid and fluid mechanics, heat transfer, dynamics and.
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Usually two activation methods are provided by the MAGNiTUDE / LND and SSQ or SolidSQUAD teams. The SSQ method is more complete but is published at longer intervals. Versions 16.2, 17.2, 18.2 and 19:. System requirements :Windows 7 (64-bit Professional and Enterprise versions)Windows 8.1 (64-bit Professional and Enterprise versions)Windows 10 (64-bit Professional and Enterprise versions)Windows Server 2008 R2 Standard Edition (64-bit), Windows HPC Server 2008 R2 (64-bit)Windows Server 2012 R2 Standard Edition22 GB on the hard drive, multiprocessing, memory> 2 GB, more> http://www.ansys.com/Support/Platform+Support.
Red Hat Enterprise 6 (6.8 & 6.9)Red Hat Enterprise 7 (7.2 & 7.3)SuSE Linux Enterprise Server 11 (SP3 & SP4)SuSE Linux Enterprise Server & Desktop 12 (SP1 & SP2).
Video tutorial for installing version 2021 R2 is located in the relevant download section.
Common Versions 16 to 19:. Two methods are presented, the first method requires the installation of a license and the second method is without the need for installation, the second method is explained;. First, with software such as DAEMON Tools or UltraISO or PowerISO, and through a virtual drive, mount Disk 1 of the software and start the installation by running the setup.exe file and then selecting the Install ANSYS Products option. Do not install ANSYS License Manager and skip the licensing step during installation by selecting Skip..
Finally, copy and replace the contents of the Local license folder in the Crack folder completely in the following default path:. C: \ Program Files \ ANSYS Inc. If the program does not install in the default path, you must run the ansyslmd.ini file in the path Crack \ Shared Files \ Licensing with Notepad and change the default license path to the installed path.
The Linux version also includes the above two methods, the steps of which are listed in the Readme file. Two methods are presented, the first method is to use License Generator and the second method is to use license and crack;. To do the first method, first right-click on the ANSYS 15.0 Calculator_DownLoadLy.exe file and run it as Run as administrator.
Then type the letter Y and press Enter. The appropriate license for your computer is created in the form of a file called license.txt. Using UltraISO or PowerISO or DAEMON Tools software, mount disk 1 and run the setup.exe file. In the initial installation window, click Install ANSYS License Manager and install the license management tool.
Then give the license.txt file created in the previous step to the program and click Continue several times.
In the second method, start installing the program and do not install the lead license. After installation, copy and replace the two cracked files in the following location:. C: \ Program Files \ ANSYS Inc \ Shared Files \ Licensing.
If you are installing software in a location other than the default drive, you must edit its address in the ansyslmd.ini file. Download section 1 – 3 GBDownload Part 2 – 3 GBDownload section 3 – 3 GBDownload section 4 – 3 GBDownload Section 5 – 2.46 GBDownload ANSYS Products 2022 R1 New Crack.
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Simulation-Driven Product Development takes engineering simulation to another level ― the unequalled depth and breadth of our software coupled with its unmatched engineered scalability, softasm.co comprehensive multiphysics foundation and adaptive architecture set our technology apart from other CAE tools.
These ANSYS Advantages add value to the engineering design process by delivering efficiency, driving innovation and reducing physical constraints, enabling simulated tests that might not be possible otherwise.ANSYS 17 System Requirements: ANSYS 17.0 is the latest released version.
The specific operating system versions supported by ANSYS 17.0 products and License Manager are documented and posted at http://www.ansys.com/Support/Platform+Support.
ANSYS 17.0 includes support for the following: – Windows 10 (64-bit) – Windows 7 (64-bit) – Windows 8.1 (64-bit) – Windows Server 2008 R2 Standard Edition (64-bit), Windows HPC Server 2008 R2 (64-bit) – Windows Server 2012 R2 Standard Edition – Red Hat Enterprise Linux (RHEL) 6.4 and 6.5 (64-bit) – SUSE Enterprise Linux Server and Desktop (SLES / SLED) 11 SP2-SP3 (64-bit).
The load is dropped to a much lower level of 27.0 KN, appropriate for a continuous cyclic operational loading.
A data probe is added to report the number of cycles for each crack increment.
A solution for an approximate 1D solution can be found using this expression:
ao is the initial crack length and
af is the final crack length.
The catch is that the Stress Intensity Factor range, is a function of crack length, so the equation has to be evaluated numerically. I have an Excel spreadsheet to perform this 1D approximation.
After I run the fatigue analysis, the probes are used to recover the Number of Cycles vs. Crack Length, as in Fig. 9.
Two ANSYS runs are carried out: a relatively coarse mesh and a finer mesh. The local element size is reduced from 0.8 mm to 0.65 mm. There is clear evidence of convergence with the life to create a 25 mm crack reducing from 3.74 E6 cycles to 3.62 E6 cycles. The 1D model provides a useful comparison with a life to 25 mm of 3.24 E6 cycles.
The convergence accuracy is based on both mesh size and initial crack step length. Both are controlled in ANSYS by the mesh size. So, finding a sufficiently fine mesh is important.
The crack extension through life is shown in Fig. 10. The stress contours are adjusted to maximum values at each step.
A hole is now inserted in the SpaceClaim model. The project is updated and automatically remeshed. No other modification is required, and the analysis is relaunched. The result of the modification is shown in Fig. 11.
The crack is now attracted to the hole and joins it on the far side from the crack origin. The crack is then arrested and there is no further extension. The crack is arrested at around 8.631 E5 cycles and the structure is damage tolerant with respect to this particular initial crack and loading.
The SpaceClaim geometry is modified by dragging the hole further away from the crack axis. The model is updated and again automatically remeshed. The results of this analysis are shown in Fig. 12.
The crack is influenced by the hole but bypasses it. Interestingly, the crack growth rate speeds up compared to a plate without a hole. The number of cycles to reach the critical crack length has dropped to 1.09 E6 cycles. This is around one-third of the total for the plate without a hole. The relationship between the hole and the crack is clearly important. The hole can arrest the crack—or speed it up!
A more arbitrary shaped hole was investigated, positioned at the same point, but elongated slightly in the vertical axis. The results of this analysis are shown in Fig. 13.
The hole attracts the crack but is not a strong enough influence to arrest it. It also acts to speed up the crack propagation further with 1.2 E5 cycles to the critical length.
Finally, a sharp notch in the hole edge was modeled to see if the crack would be attracted. This is shown in Fig. 14.
The sharp notch does attract and arrest the crack. It now takes 6.76 E5 cycles to reach this point. The notch is intercepted partway along its length. This is shown more clearly in the displacement plot, which is inset in the last frame of Fig. 13. Experimenting with the notch shows there is a critical length to attract the crack to an arrested state. Below that length the notch acts to accelerate the crack.
The workflow to set up the crack and define the fracture parameters is straightforward. The direct interface with SpaceClaim geometry allows for rapid “what-if” studies. This is a versatile tool and I have only shown one crack type.
The Arbitrary Crack and Semi-Elliptical Crack look useful in creating cracks in more complex geometry. The other fracture solution methods, Interface Delamination and Contact Debonding, provide solutions for pre-defined crack paths, such as along bond lines.