I think it's much better to learn newcomers the right terms and
nomenclature, instead of starting with easier terms that are more confusing.
This will prevent a lot of misconceptions.
So Ren:
There are two values that describe a airfoil (a wing section, or rib), these
are the thickness and camber. Thickness is the distance from the upper to
the lower surface of the rib, generaly we speak about the maximum thichness.
For example, a thickness of 5% at a 20cm chord (length of a rib) means a
maximum thickness of 1cm.
The camberline represents a line axactly inbetween the upper and lower
surface. This line has a slight curvature. The highest point of this line in
the max. camber and is also denoted as a percentage of the chord.
You can see these terms also in the next picture:
http://airfoils.worldofkrauss.com:8888/images/airfoil_definitions.png
Kevin
2010/1/15 ray_harlan <rbharlan_at_comcast.net>
>
>
> For a newcomer, I think we should be talking about max rib height. Since
> the airfoil section essentially has zero thickness, then this height is the
> same as camber. But that is an aero engineering term that modellers may not
> be familiar with. The commonality of modelling terms may be a bit different
> on the other side of the pond.
>
> Ray
>
>
> --- In Indoor_Construction_at_yahoogroups.com<Indoor_Construction%40yahoogroups.com>,
> "John Barker" <john.barker783_at_...> wrote:
> >
> > Ray and Fred
> > I don't want to be picky but should we be talking about camber instead of
> thickness. Those of us who have been dabbling in these things for years have
> shorthand ways of talking that we all understand but Ren, being a newcomer,
> may be puzzled, particularly after the correction from degrees to percent.
> > John
> >
>
>
>
Received on Fri Jan 15 2010 - 06:17:08 CET
