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

Blade Element Analysis

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

Reply
 
LinkBack Thread Tools Display Modes
Old   June 17, 2008, 02:35
Default Blade Element Analysis
  #1
Kwon
Guest
 
Posts: n/a
Is it possible to calculate or estimate the local pressure coefficient of the rotating blade surface of a helicopter using the Blade Element Theory(BET) or Blade Element Momemtum Theory(BEMT)? If possible, please recommend the proper references.

Thank you!
  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


Similar Threads
Thread Thread Starter Forum Replies Last Post
autoPatch error, mesh quality related...? Alexvader OpenFOAM 0 October 6, 2011 17:57
Mathematical analysis of the cyclic stresses in the Wind Turine Blade Root milindashokshende Main CFD Forum 1 May 26, 2010 10:36
mesh file for flow over a circular cylinder Ardalan Main CFD Forum 6 April 17, 2010 23:40
stress analysis of a rotating beam(wind blade) Cheyannne ANSYS 0 October 19, 2009 17:06
element with negative volume - FSI analysis Seb CFX 3 May 22, 2005 19:04


All times are GMT -4. The time now is 17:39.