[ANSYS Meshing] Structured O-type Grid Around NACA Airfoil -- CFD Online Discussion Forums

May 4, 2019, 19:52	Structured O-type Grid Around NACA Airfoil	#1
@sher New Member Asfand Yaar Sher Join Date: Jan 2019 Posts: 8 Rep Power: 7	I'm trying to make a structured O-type grid around NACA airfoil. But I'm unable to do so as I don't know the exact values of biasing factor, number of elements etc. I have done the tutorial of Structured C-type mesh.

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
wallHeatFlux utility for an incompressible case	Mr.Jingles	OpenFOAM Post-Processing	67	April 6, 2023 03:25
Inlet patch problems	martyn88	OpenFOAM Running, Solving & CFD	6	April 21, 2017 18:34
Floating point exception error	lpz_michele	OpenFOAM Running, Solving & CFD	53	October 19, 2015 02:50
LES supersonic free jet	martyn88	OpenFOAM	22	April 17, 2015 06:00
Strange high velocity in centrifugal pump simulation	huangxianbei	OpenFOAM Running, Solving & CFD	26	August 15, 2014 02:27

All times are GMT -4. The time now is 10:07.