----- Original Message -----
Sent: Friday, October 21, 2005 2:53
PM
Subject: [FlyRotary] Re: NACA
scoops
Ernest,
Mockups are only in my mind at this time........I
would like to see your Javafoil info
as I think it would be helpful to exit cooling air at or near separation
point if I am
correct in what I think I know (very little) about the subject !! I am on
dialup , can I
get you to burn me a cd !! E-mail me privately with your address and
I will send cost
and postage......
--
Kelly Troyer
Dyke
Delta/13B/RD1C/EC2
--------------
Original message from Ernest Christley <echristley@nc.rr.com>:
--------------
> Kelly Troyer wrote:
>
> >
Inlet lip will not protrude enough to use as step
> > if I follow
NACA report 743 (subject to change if I need to modify lip
> >
from 743 shapes).
>
>
> Kelly, I think that to get the
most from this report, you'll need to use
> something like Javafoil
to compare the transition and seperation points
> of the NACA 23017
(which was used in the report) against the Delta's.
> I've got those
if you're interested. What I think is particulary
> interesting to
see is comparing the configurations where the efficiency
> jumps off
the charts to where the natural transition and seperation
> points
occur on the wing sections.
>
> Thomas, I don't think there is