|
[Sponsors] |
Convergence failed using unrealistic airfoil in xfoil |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
February 28, 2019, 11:45 |
Convergence failed using unrealistic airfoil in xfoil
|
#1 |
New Member
Pratik
Join Date: Oct 2018
Posts: 11
Rep Power: 8 |
In optimization process when unrealistic airfoil came it can't analysis in xfoil due to convergence issue. How to I get result for unrealistic airfoil using xfoil (for finding value of cl and cd.)
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Upload Airfoil Coordinates on Xfoil Help | rome | Main CFD Forum | 0 | August 13, 2017 03:35 |
how to use xfoil to compute airfoil displacement thickness? | jeromechen | Main CFD Forum | 1 | August 21, 2011 07:47 |
2D SST Simulation Airfoil - Convergence Problem | Kraemer | CFX | 10 | April 16, 2011 08:22 |
Convergence Criteria - airfoil sim. | Andres Bernal | CFX | 2 | December 18, 2006 19:57 |
user defined function | cfduser | CFX | 0 | April 29, 2006 11:58 |