-
-
April 24, 2020 at 1:27 pm
masaziz
Subscriberi guys, now I'm currently working with CFX and Static Structural. I'm doing research on fatigue-life from Propeller KP-505. When I'm importing the pressure from CFX to Static Structural using the Imported Pressure feature, why the red vortex/arrow only appears on 3 blades (red circles), and the 2 other blades don't have the red vertex/arrow (pink circles)? Can somebody explain to me why this is happening?
I attach the screenshot below.
Thanks!
-
April 24, 2020 at 7:16 pm
Aniket
Forum ModeratorAnsys staff can not download images on the student portal, so if you want to reach a larger audience to get answers from, please insert the images inline. Also, did you check the import summary? is the exported result mesh and the mesh it is mapped on closely matchig?
-Aniket
How to access Ansys Online Help Document
How to show full resolution image
Guidelines on the Student Community
How to use Google to search within Ansys Student Community
Â
-
April 24, 2020 at 9:30 pm
-
April 25, 2020 at 7:03 am
Aniket
Forum ModeratorWhat do you see in the Imported Load transfer summary? It should open in the worksheet showing the detailed summary. Have you crosschecked the results in CFX if those are matching with what is being mapped? Don't pay attention to colours check the values of pressures.
-Aniket
How to access Ansys Online Help Document
How to show full resolution image
Guidelines on the Student Community
How to use Google to search within Ansys Student Community
Â
-
- The topic ‘Contour on Imported Pressure’ is closed to new replies.
- LPBF Simulation of dissimilar materials in ANSYS mechanical (Thermal Transient)
- Convergence error in modal analysis
- APDL, memory, solid
- Meaning of the error
- How to model a bimodular material in Mechanical
- Simulate a fan on the end of shaft
- Nonlinear load cases combinations
- Real Life Example of a non-symmetric eigenvalue problem
- How can the results of Pressures and Motions for all elements be obtained?
- Contact stiffness too big
-
4177
-
1487
-
1363
-
1194
-
1021
© 2025 Copyright ANSYS, Inc. All rights reserved.
.jpg?width=690&upscale=false)

