-
-
September 12, 2023 at 11:17 am
IKUTA Motoki
SubscriberI am a university student who has started using Ansys.
I would like to create and analyze an airplane wing using NACA0021, but the mesh of the trailing edge of the wing cannot be divided properly.
If I make the entire mesh too fine to allow mesh division of the trailing edge, the number of meshes will become too large.
I am thinking that if I can make only the mesh near the trailing edge finer, I can solve this problem, but I don't know how.
I would like someone to tell me how to do this.
Best regards,
Motoki -
September 12, 2023 at 12:42 pm
Rob
Forum ModeratorPlease have a look at the courses in Learning and in the tutorials in the Mesher Help system.Â
-
September 12, 2023 at 12:53 pm
Federico
Ansys EmployeeWhat are you using for meshing? Agree with Rob, there are several courses on this topic.
-
Viewing 2 reply threads
- The topic ‘Question about wing mesh division’ is closed to new replies.
Ansys Innovation Space
Trending discussions
- air flow in and out of computer case
- Varying Bond model parameters to mimic soil particle cohesion/stiction
- Eroded Mass due to Erosion of Soil Particles by Fluids
- I am doing a corona simulation. But particles are not spreading.
- Guidance needed for Conjugate Heat Transfer Analysis for a 3s3p Li-ion Battery
- Centrifugal Fan Analysis for Determination of Characteristic Curve
- Issue to compile a UDF in ANSYS Fluent
- JACOBI Convergence Issue in ANSYS AQWA
- affinity not set
- Resuming SAG Mill Simulation with New Particle Batch in Rocky
Top Contributors
-
3882
-
1414
-
1241
-
1118
-
1015
Top Rated Tags
© 2025 Copyright ANSYS, Inc. All rights reserved.
Ansys does not support the usage of unauthorized Ansys software. Please visit www.ansys.com to obtain an official distribution.