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

Airfoils and lift compared to air density and TE

Register Blogs Members List Search Today's Posts Mark Forums Read

Reply
 
LinkBack Thread Tools Display Modes
Old   May 4, 2006, 03:31
Default Airfoils and lift compared to air density and TE
  #1
Jens
Guest
 
Posts: n/a
Hi,

I am studing a flare system with compbustion and high speed flow using CFD simulation. I would like to compared the flow in the vicinity of the flare plume to data regarding the stability of an airfoil.

That means I am looking for what range is a generel airfoil of a airplane (small airplane) stabel.

Like a minimum limite of the air density ?

And what levels should the turbulence kinetic energy be below ?

Does anyone knows were to find such information ???

Thanks on advance.

Kind regards

Jens
  Reply With Quote

Reply

Thread Tools
Display Modes

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 On
Pingbacks are On
Refbacks are On



All times are GMT -4. The time now is 12:34.