CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > FloEFD, FloWorks & FloTHERM

Help me! Non-stationary calculation aircraft

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   May 23, 2020, 06:27
Angry Help me! Non-stationary calculation aircraft
  #1
New Member
 
Sergey
Join Date: May 2020
Posts: 2
Rep Power: 0
Pups is on a distinguished road
Hi everyone!
Need help, pleease.
Please tell me whether it is possible in FloEFD to simulate the descent of the device in the atmosphere with a change in atmospheric parameters in height.

PS if it doesn’t complicate, describe as detailed as possible, I can’t understand how to solve the unsteady problem correctly
Pups is offline   Reply With Quote

Old   June 30, 2020, 08:39
Default
  #2
Disabled
 
Join Date: Jul 2009
Posts: 616
Rep Power: 24
Boris_M will become famous soon enough
Hi Sergey,

Yes, it is possible.
First of course you will need a transient project setting. Of course you will need to know the overall time of your descent and the height change over the time.
You can then change the "thermodynamic parameters" in the Initial and ambient conditions of the Wizard/General settings to "Altitude". The parameters here are based on the standard atmosphere with a temperature deviation. You can then set the height as a dependency (see the button at the bottom) and select for example "F(time) -Table" where you can enter your data of the height over the time.

Regards,
Boris
Boris_M is offline   Reply With Quote

Reply

Tags
aerodynamic, aircraft design, condition missing, hypersonic flow, rocket


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
Increase in CPU number during the FIRE calculation amin_u50 AVL FIRE 0 August 6, 2014 09:34
Calculation of initial k for RAS turbulence models shipman OpenFOAM 1 August 28, 2013 04:52
DICPCG calculation don't converge (interFoam) Kaquesang OpenFOAM Running, Solving & CFD 0 November 16, 2012 21:05
SITVC calculation cfdzak Main CFD Forum 0 July 18, 2012 03:50
[ICEM] Annoying mesh holes on an aircraft Santos-Dumont ANSYS Meshing & Geometry 2 March 2, 2012 09:13


All times are GMT -4. The time now is 04:26.