|
[Sponsors] |
September 28, 2016, 11:44 |
Hydrofoil wing in fluent
|
#1 |
New Member
Martijn
Join Date: Apr 2016
Posts: 10
Rep Power: 10 |
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 |
|
September 30, 2016, 10:30 |
|
#2 | |
New Member
Jobin
Join Date: Sep 2016
Posts: 5
Rep Power: 10 |
Quote:
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. |
||
September 30, 2016, 10:45 |
|
#3 |
New Member
Martijn
Join Date: Apr 2016
Posts: 10
Rep Power: 10 |
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. |
|
September 30, 2016, 10:50 |
|
#4 |
New Member
Jobin
Join Date: Sep 2016
Posts: 5
Rep Power: 10 |
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. |
|
Tags |
airfoil 3d, fluent, hydrofoil, naca |
|
|
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 |