The data on the foil is for a 2D section of infinite span. Real wings are not infinite in length. It is not easy to get a Cl over 1 for a single element wing.
I suggest you use 0.7 for a single wing with realistic span.
On 10/01/2016, at 12:44 AM, "taladorwood@yahoo.com.au [harryproa]" <harryproa@yahoogroups.com.au> wrote:
Look at the generic 0012 foil here NACA0012H for VAWT from Sandia report SAND80-2114 (naca0012h-sa)
__._,_.___
Posted by: Rick Willoughby <rickwill@bigpond.net.au>
| Reply via web post | • | Reply to sender | • | Reply to group | • | Start a new topic | • | Messages in this topic (68) |
.