Home > Forums > Software User Forums > ANSYS > ANSYS Meshing & Geometry

[ANSYS Meshing] 2D Airfoil Meshing Problem for Leading Edge Cylinder

Updated Threads

Reply

Search this Thread

June 30, 2021, 22:54	2D Airfoil Meshing Problem for Leading Edge Cylinder	#1
roy_003 New Member Debasish Roy Join Date: Jan 2019 Posts: 3 Rep Power: 7	Hello! I am trying to do a 2D analysis of a NACA 4412 Airfoil with a Leading Edge Rotating Cylinder. I followed the process of [ this video ] to get a structured mesh. But the gap between cylinder and airfoil seems to be problematic. Please give some suggestions. I have attached Screenshots. 1 Zoomed.jpg 1.JPG Mesh.jpg

Reply

Tags

airfoil, ansys meshing, fluent, meshing 2d

« Previous Thread | Next Thread »

Posting Rules
You may not post new threads You may not post replies You may not post attachments You may not edit your posts BB code is On Smilies are On [IMG] code is On HTML code is Off Trackbacks are Off Pingbacks are On Refbacks are On Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
[Gmsh] gmshToFoam generates patches with 0 faces and 0 points	Simurgh	OpenFOAM Meshing & Mesh Conversion	4	August 25, 2023 07:58
ANSYS 2020 R2 - Airfoil meshing trailing edge problem	Addkkqw	ANSYS	1	October 22, 2020 06:56
2D FFD Optimization	RLangtry	SU2	2	August 5, 2014 09:48
[ANSYS Meshing] problem about the geometry and meshing of the airfoil	yileihe1989	ANSYS Meshing & Geometry	2	February 24, 2013 06:18
Gambit - meshing over airfoil wrapping (?) problem	JFDC	FLUENT	1	July 11, 2011 05:59

All times are GMT -4. The time now is 16:59.