CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT

Hydrofoil wing in fluent

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   September 28, 2016, 11:44
Default Hydrofoil wing in fluent
  #1
New Member
 
Martijn
Join Date: Apr 2016
Posts: 10
Rep Power: 10
wind_tunnel_contraction is on a distinguished road
Hello all,

Currently I am working on a hydrofoil wing. I already calculated the lift en drag (coefficients) using XFoil. A software program for all kinds of airfoils. Now I wanted to know the lift and drag of the complete wing. This includes:

- two elliptical wing sections at the sides
- a middle wing section with same chord-length
- two nacelles to connect the wings to the struts and to house the bearings for pitch control of the wing sections.

As I already know the drag of the struts, I am only interested in the lift and drag of the complete wing including 2 nacelles.

Earlier, I used Ansys Fluent for the flow of a wind-tunnel contraction. Now I encounter a few problems:

- how to mesh this profile sufficiently (the enclosed box and the hydrofoil with nacelles)?

- which Turbulence model and turbulence values should I choose in water? Or is laminar flow sufficient for a low speed (12m/s max) foil?

Thank you in advance,

Martijn
wind_tunnel_contraction is offline   Reply With Quote

Old   September 30, 2016, 10:30
Default
  #2
New Member
 
Jobin
Join Date: Sep 2016
Posts: 5
Rep Power: 10
Poompil is on a distinguished road
Quote:
Originally Posted by wind_tunnel_contraction View Post
- which Turbulence model and turbulence values should I choose in water? Or is laminar flow sufficient for a low speed (12m/s max) foil?
The second part of this depends on your Reynolds number.
http://airfoiltools.com/calculator/r...&yt0=Calculate

For a speed of 12 m/s, you'll essentially need to work in the turbulent regime, for any appreciable chord.
Poompil is offline   Reply With Quote

Old   September 30, 2016, 10:45
Default
  #3
New Member
 
Martijn
Join Date: Apr 2016
Posts: 10
Rep Power: 10
wind_tunnel_contraction is on a distinguished road
Thank you for your answer,

which turbulent model should I use? I saw aerofoils with K-epsilon model. The problem with this model are the values for the parameters. How can I obtain these values?

Very low Turbulence Intensity value is assumed, but how low? The same for the viscosity ratio.

The chord length is approximately 0.08m and with a range of 5-12m/s the reynolds range is 5e5 to 1e6.
wind_tunnel_contraction is offline   Reply With Quote

Old   September 30, 2016, 10:50
Default
  #4
New Member
 
Jobin
Join Date: Sep 2016
Posts: 5
Rep Power: 10
Poompil is on a distinguished road
I don't know enough to answer all your questions, but yes, picking turbulence parameters is indeed a difficulty.

I would suggest the following approaches:
1) Look at literature on hydrofoils of similar scale and see if you can wean any information from there.
2) This page has some good guidelines on choosing turbulence parameters.
Poompil is offline   Reply With Quote

Reply

Tags
airfoil 3d, fluent, hydrofoil, naca


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
fluent subsonic wing analysis problem fatihcoban FLUENT 0 August 3, 2016 10:41
Wing Aerodynamics Fluent OF 15 comparison maddalena OpenFOAM Running, Solving & CFD 85 August 20, 2013 11:36
[snappyHexMesh] Meshing 3D wing (hydrofoil) fails klausb OpenFOAM Meshing & Mesh Conversion 0 December 28, 2011 15:26
mesh missing after import in fluent morteza08 FLUENT 0 July 23, 2010 03:22
Wing tip vortices using Fluent Jainy FLUENT 3 August 22, 2005 20:13


All times are GMT -4. The time now is 11:02.