|
[Sponsors] |
![]() |
![]() |
#1 |
New Member
Sridhara B C
Join Date: Apr 2017
Posts: 1
Rep Power: 0 ![]() |
Hi all I am doing Flutter analysis of compressor blade, I am using ANSYS workbench for this.
Here i am giving the steps carried out for this analysis. 1. Modal analysis for 35350 rpm speed 1. Steady state analysis using CFX. 2. Unsteady case for flutter analysis by importing the mode shapes from modal analysis these are the major 3 steps followed, for flutter analysis we are going for Transient blade row method - Fourier transformations. I am getting negative volume error, even though mesh is fine, and time steps also large, please give some suggestions to overcome this |
|
![]() |
![]() |
![]() |
![]() |
#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,933
Rep Power: 145 ![]() ![]() ![]() ![]() |
||
![]() |
![]() |
![]() |
Tags |
cfx-flutter analysis |
Thread Tools | Search this Thread |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Flutter Analysis | egw.uab | STAR-CCM+ | 3 | October 12, 2016 14:39 |
Need help flutter analysis research | egw.uab | Main CFD Forum | 0 | October 7, 2016 11:05 |
wing flutter analysis | varghese9 | ANSYS | 0 | January 27, 2015 23:53 |
Flutter analysis on a wing | samcfd | FLUENT | 0 | July 30, 2012 01:27 |
Flutter analysis | sulakshanarya | CFX | 0 | February 20, 2012 06:49 |