|
[Sponsors] |
June 17, 2008, 03:35 |
Blade Element Analysis
|
#1 |
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! |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
mesh file for flow over a circular cylinder | Ardalan | Main CFD Forum | 7 | December 15, 2020 14:06 |
autoPatch error, mesh quality related...? | Alexvader | OpenFOAM | 0 | October 6, 2011 18:57 |
Mathematical analysis of the cyclic stresses in the Wind Turine Blade Root | milindashokshende | Main CFD Forum | 1 | May 26, 2010 11:36 |
stress analysis of a rotating beam(wind blade) | Cheyannne | ANSYS | 0 | October 19, 2009 18:06 |
element with negative volume - FSI analysis | Seb | CFX | 3 | May 22, 2005 20:04 |