[overture] Re: NACA airfoil grid
- From: "Adnan Qamar" <Adnan.Qamar@xxxxxxxxxxxx>
- To: "overture@xxxxxxxxxxxxx" <overture@xxxxxxxxxxxxx>
- Date: Sun, 1 Sep 2013 07:20:14 +0000
Hi Bill,
Yes, I have gone through the example files. There is no problem making a grid.
However, I have issues in fixing the aspect ratio at the trailing edge.
Best,
Adnan
Adnan Qamar, PhD
Mechanical Engineering,
Physical Sciences and Engineering Division,
Building 4, Room 3216,
4700 King Abdullah University of Science and Technology (KAUST),
Thuwal 23955-6900, KSA.
Email: Adnan.Qamar@xxxxxxxxxxxx
Ph: 966-2-8084896
Fax: 96628021077@xxxxxxxxxxxxxxxx
________________________________
From: overture-bounce@xxxxxxxxxxxxx [overture-bounce@xxxxxxxxxxxxx] on behalf
of Bill Henshaw [henshaw@xxxxxxxx]
Sent: Friday, August 30, 2013 9:41 PM
To: overture@xxxxxxxxxxxxx
Subject: [overture] Re: NACA airfoil grid
Hi Adan,
Sorry but I haven't looked at your grid yet. There are, however, some
example grids for 2D
airfoils. Have you tried just extruding those?
...Bill
On 08/28/2013 04:54 AM, Adnan Qamar wrote:
Hi Bill,
I am trying to generate a 3D mesh over an airfoil surface. I am using
hyperbolic grid generation with smothning operation to generate the mesh. I
want to control aspect ratio at the trailing edge of the airfoil. Can you
please suggest me how to control the aspect ration at the trailing edge of the
airfoil (contract line spacing along the cut line on either side) . Attached
is the cmd file I am using.
Best,
-Adnan
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