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

Optimal pitch angle for the blades of the HAWT

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   July 31, 2019, 04:11
Lightbulb Optimal pitch angle for the blades of the HAWT
  #1
New Member
 
Volodymyr Klymko
Join Date: Nov 2014
Location: Lviv, Ukraine
Posts: 6
Rep Power: 12
Volodymyr is on a distinguished road
Send a message via Skype™ to Volodymyr
Dear All,

If anyone could assist me with following I would be very thankful.

My question is related to the optimal pitch angle when wind rotor blades are not moving.

The power extracted from the wind is equal to 0.5*rho*A*Cp(lambda)*velocity^3, where rho - air density, A - area of the rotor (pi*radius^2 for HAWTs, 2*radius*blade_height for VAWTs), Cp(lambda) - rotor power coefficient which shows the effectiveness of the turbine at specific lambda. Lambda is non-dimensional operator which shows the ratio of linear velocity of the blade which is angular_velocity*radius to the air velocity.

For each air velocity value there is a optimal angular velocity, so the wind rotor could operate at optimal lambda, thus to have maximum rotor power coefficient. It works just fine when wind rotor is spinning and blades have some linear velocity. Changing the pitch angle it is possible to change the angle of attack, so the rotor will either decelerate or accelerate.

Here comes the question:

if wind rotor is not spinning, so linear velocity equals to zero. If linear velocity is zero, than lambda is also zero - thus Cp(lambda) is zero. Which pitch angle the wind blades have to be set to, so they will start to rotate? I am more curious about twisted blades, since one pitch angle will result in different angles of attack along the length of the blade, because blade is twisted.

Thank you so much.
Volodymyr is offline   Reply With Quote

Reply

Tags
angle of attack, blades, hawt, pitch angle


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
Using a field function in changing the pitch angle of helicopter blades Donegalstevie Siemens 0 June 26, 2014 10:27
pitch angle keeper CFX 2 October 24, 2013 03:26
[Netgen] Import netgen mesh to OpenFOAM hsieh OpenFOAM Meshing & Mesh Conversion 32 September 13, 2011 06:50
Divergence problem when airfoil exceed pitch angle zonexo Main CFD Forum 2 April 4, 2007 05:22
Yaw and Pitch angle for gasturbflow Haloejsa Main CFD Forum 0 November 5, 2003 16:20


All times are GMT -4. The time now is 22:14.