CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT

Supersonic Flow Over Flat Plate using Ansys-Fluent

Register Blogs Community New Posts Updated Threads Search

 
 
LinkBack Thread Tools Search this Thread Display Modes
Prev Previous Post   Next Post Next
Old   October 4, 2019, 02:04
Default Supersonic Flow Over Flat Plate using Ansys-Fluent
  #1
New Member
 
Venkata Raghavendra Nandagiri
Join Date: Jan 2013
Location: Bengaluru
Posts: 1
Rep Power: 0
Venkata R.Nandagiri is on a distinguished road
Hello, has anyone successfully simulated Anderson Ch.10 test case of Supersonic flow over flat plate, using Ansys-Fluent? If so, please let me know what to take for:

1) The plate geometry/dimensions and the mesh dimensions
2) Boundary conditions
3) Flow solver (convective flux, etc)
4) Time step
5) Any other important info related to the Fluent simulation

Please confirm if the results of surface pressure distribution as a function of distance from the leading edge obtained using Ansys-Fluent, match those given in Anderson book.
Venkata R.Nandagiri is offline   Reply With Quote

 


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
Flow over a heated flat plate: non-physical solution Sushobhan OpenFOAM Running, Solving & CFD 0 May 4, 2018 23:43
heat transfer with RANS wall function, over a flat plate (validation with fluent) bruce OpenFOAM Running, Solving & CFD 6 January 20, 2017 06:22
Supersonic flow over flate plate SAz_ID FLUENT 9 August 17, 2014 14:09
Question about Laminar flow over flat plate in FLUENT gaoyitong FLUENT 0 November 26, 2012 22:51
problem in turbulent flow over flat plate with stagnation point mb.pejvak Main CFD Forum 0 September 12, 2012 21:25


All times are GMT -4. The time now is 11:23.