|
[Sponsors] |
[DesignModeler] Changing airfoil thickness for DOE analysis |
![]() |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
![]() |
![]() |
#1 |
New Member
Soheil
Join Date: Mar 2014
Location: Helsinki
Posts: 21
Rep Power: 12 ![]() |
Hi.
I'm using ANSYS DesingXplorer for optimizing a wing. Wing root chord length is 1.21m and tip chord is 0.234m. One of my input parameters for DOE is airfoil thickness to chord ratio (t/c). I'm wondering how can I change airfoil thickness without any change to chord length? is it even possible or it's just the only way? for example, I'm changing it from t/c=0.1 to t/c=0.06. but root chord changes from 1.21 to 0.731, respectively. Airfoil is naca64a210. Thank you. |
|
![]() |
![]() |
![]() |
Tags |
airfoil, design modeler, doe, thickness |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Problem with airfoil shape optimization | robyTKD | SU2 Shape Design | 7 | March 7, 2022 16:18 |
The boundary layer thickness on an airfoil | Nick R | Main CFD Forum | 5 | October 23, 2013 10:25 |
Problem with restart solution in shape_optimization.py | robyTKD | SU2 Shape Design | 21 | May 29, 2013 09:26 |
how to use xfoil to compute airfoil displacement thickness? | jeromechen | Main CFD Forum | 1 | August 21, 2011 06:47 |
Changing CFX.def in WorkBench Parametric analysis | sodjaj | ANSYS | 1 | August 23, 2010 10:04 |