|
[Sponsors] |
Information propagation in a subsonic compressor |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
May 1, 2019, 15:34 |
Information propagation in a subsonic compressor
|
#1 |
Senior Member
Join Date: Aug 2012
Posts: 268
Rep Power: 14 |
Could someone please explain about the information propagating in a subsonic compressor?
As seen in the image, I have put numerical probes in the IGV, Rotor, Stator and casing treatment. My question is that since information in a subsonic flow regime propagates in upstream direction, should the passing frequencies of the rotor, the stator and the casing treatment or their harmonics appear in the probe I placed in the IGV? How about the casing treatment? |
|
May 1, 2019, 18:56 |
|
#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
I would imagine so. But whether those frequencies are strong and significant enough to be seen between all the other noise is another matter.
__________________
Note: I do not answer CFD questions by PM. CFD questions should be posted on the forum. |
|
May 2, 2019, 01:57 |
|
#3 |
Senior Member
Join Date: Aug 2012
Posts: 268
Rep Power: 14 |
How about the casing treatment?
Can the the passing frequency of IGV appear in the probe I placed in the casing treatment? Does it mean that every component in a subsonic compressor feel the presence of other components regardless of their positions? |
|
May 2, 2019, 02:41 |
|
#4 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,703
Rep Power: 143 |
Theoretically, yes. But again, whether the signal from far away features is swamped by noise from other closer features is another matter.
__________________
Note: I do not answer CFD questions by PM. CFD questions should be posted on the forum. |
|
May 17, 2019, 11:19 |
|
#5 |
Senior Member
Join Date: Aug 2012
Posts: 268
Rep Power: 14 |
Which one of instanteous or averaged data should be used to capture blade passing frequency?
I have used a probe which recordrs absoulte pressure. When I analyse the FFT of this probe, I get half or less than the half of the blade passing frequency. Why does this happen? |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[TurboGrid] Turbocharger Compressor Wheel Meshing | aymen_a22 | ANSYS Meshing & Geometry | 0 | March 20, 2013 10:27 |
Compressor Blade Analysis in Ansys CFX | LynchMobster47 | Main CFD Forum | 0 | April 10, 2012 22:43 |
Terrible Mistake In Fluid Dynamics History | Abhi | Main CFD Forum | 12 | July 8, 2002 09:11 |
Inviscid Drag at subsonic, subcritical Mach # | Axel Rohde | Main CFD Forum | 1 | November 19, 2001 12:19 |
CFD Problem: volumetric compressor | Gabriele Velenich | Main CFD Forum | 2 | July 2, 2001 08:15 |