CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > General Forums > Main CFD Forum

supersonic flow past flat plate

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   July 28, 2007, 20:47
Default supersonic flow past flat plate
  #1
shuo
Guest
 
Posts: n/a
Hi

I am simulating it by solving the conservation form of the Navier-Stokes equations using MacCormick's method. I am solving it at Ma 4, Re 700. The velocity profile looked reasonable (compared with vanDriest) but the pressure and density profile had sharp oscillations across the boundary layer(BL). The temperatue profile was smooth. Is there any way I can minimise the oscillations(artificial viscosity?).

ALso for the initial conditions, I had to use a assume a linear BL velocity profile over an equivalent subsonic Blasius flow. If I assumed uniform velocity everywhere except at the plate, the solution blows up immediately. Is it because of the huge velocity difference at the surface nodes? For hypersonic flows Ma > 6 the solution always blow up.

Cheers Shuo
  Reply With Quote

Reply


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
compressible laminar flow over flat plate varunjain89 Main CFD Forum 19 April 18, 2019 07:07
Experimental paper for flow over flat plate Sid Main CFD Forum 3 October 8, 2008 12:45
Flow over a flat plate & Flow over a cylinder cfdxue Main CFD Forum 0 November 27, 2007 00:26
BIg BIg Problems....SUPERSONIC FLOW OVER A FLAT PL edison Main CFD Forum 7 October 11, 2005 10:34
results for flow past flat plate normal to flow lisa Main CFD Forum 2 August 30, 2005 17:36


All times are GMT -4. The time now is 18:25.