CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > Siemens > STAR-CCM+

nozzle thrust issue

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   August 26, 2020, 03:57
Default nozzle thrust issue
  #1
New Member
 
huang,wei-hsin
Join Date: Aug 2020
Location: TAIWAN,R.O.C.
Posts: 3
Rep Power: 5
stonecold1634 is on a distinguished road
https://i.imgur.com/o0WgnTu.jpg

Hello,I am doing the simulation of a 2D nozzle.As you can see in the picture,
exit jet is curved by the second inject flow,so , there will be a curve angle.

And there are some problems happened in "THRUST" evaluate:

1.Is build "probe" the proper method to calculate thrust?
2. How to get Fx and Fy?(calculate curved angle)

PLS help me to check the procedure of parameter thrust.
stonecold1634 is offline   Reply With Quote

Old   September 1, 2020, 08:28
Default
  #2
Senior Member
 
Matt
Join Date: Aug 2014
Posts: 947
Rep Power: 17
fluid23 is on a distinguished road
Your question is not totally clear, can you rephrase it? In general, to get forces you would select your wall boundaries as inputs to a force report (or force reports if you want different directions, x and y).
fluid23 is offline   Reply With Quote

Reply

Tags
nozzle thrust


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
kOmegaSST Boundary Conditions for Supersonic Nozzle shang2 OpenFOAM Running, Solving & CFD 2 September 17, 2018 13:06
3D Thrust Vectoring Nozzle rhoCentralFoam problem AleQ95 OpenFOAM Running, Solving & CFD 1 May 3, 2018 16:43
Issue: Nozzle Discharge Coefficient LiamH FLUENT 3 February 25, 2017 17:04
[ICEM] Troubleshooting Wall Inflation Issue for a 2D Nozzle cfmontes ANSYS Meshing & Geometry 1 May 14, 2015 18:13
C-D nozzle supersonic jet boundary Gland FLUENT 4 May 24, 2012 00:25


All times are GMT -4. The time now is 04:09.