Forum

Important Notice for New User Registrations

To combat an increasing number of spam and bot registrations, we now manually approve all new user registrations. While this may cause a delay until your account is approved, this step is essential to ensure the quality and security of this forum.

To help us verify your registration as legitimate, please use a clear name as user name or an official email address (such as a work, university, or similar address). If you’re concerned that we may not recognize your registration as non-spam, feel free to email us at with a request to approve your username.

Please or Register to create posts and topics.

The output of the wake

Dear all,

I want to know whether there are channels to output wake results, such as Y-Z wake plane velocity distributed along the X-axis, vorticity distribution, shedding vorticity, trailing vorticity and other similar parameters.

Thanks

Hi,

wake velocity data can be exported via “velocity cut planes”.

At first you need to activate the option in the dock – then you can create and export velocity cut planes for a completed simulation.

If you store the replay of a simulation you can export cut planes at each stored timestep. Cut planes can be exported to .txt files or .vtu files that can directly be inspected with Paraview.

BR,

David

Uploaded files:
  • You need to login to have access to uploads.
robytian has reacted to this post.
robytian

Thank you for your answer, this feature is really great, give you a thumbs up.

Dear David,

Hello, may I ask:

I divided the blade into 18 panels. Through calculation, I obtained the bound vorticity of 0 to 17 panels on the blade 1.

Through the simulation image, I found two trailing vortex lines pulled out from the blade tip. I would like to ask whether the bound vortexes in section 17 are located in the blue or yellow position of the image I drew.

In addition, I would like to know how these two trailing vortex lines are calculated through the bound vortexes. Is it the attachment vortex of panel 17 minus panel 16 that gives the trailing vortex between them? What is the trailing vortex at the blade tip?

Uploaded files:
  • You need to login to have access to uploads.

Hi,

I think I dont really understand your question, but please have a look at our documentation: https://docs.qblade.org/src/theory/aerodynamics/lifting_line/lifting_line.html to clarify this.

Best,

David

Hi David,

Through calculation, I find that the longer the simulation time is, the longer the distance of wake along x will be, but it will be truncated at a certain distance.

I want to get the wake field of 10 times the rotor diameter through simulation, and get the Y-Z plane at each time the impeller diameter. How to set it?

 

Dear David

Could you please help me to answer the above questions?

Thank you very much.

Best wishes,

Yinong

Hi Rob,

please check out the documentation on the vortex wake settings here: https://docs.qblade.org/src/user/turbine/aerodynamic.html#free-vortex-wake-parameters

There all parameters regarding the vortex wake settings (and how the cut-off length is affected) are explained. When running the sim you should store the replay of the simulation. After the simulation is finished you can then export the wake data at any location for all timesteps of the simulation.

BR,

David

robytian has reacted to this post.
robytian

Scroll to Top