Paul, no thread, article by Lewis in Kitplanes. Just a thank
you from me, he was promoting the rotary!
Lewis, thanks for the recent Kitplanes read,
Steve Carlisle
I second that. Illustrates the real essences of the real
experimental air craft
designing and building hobby.
Not the pre-punched Ramp Vermin stuff.
It is in the October issue. I'll scan it in a month or two.
I am not surprised the Quickie with the wheels at the wings
tips had on the
ground directional stability problems. Half the drag on a car
at 50 mph
is rolling resistance. That in turn is a function of load. If
you load one wheel
at the end of wing more than the wheel at the other end of the
wing nothing is
going to keep that airplane going straight. That is why a lot
of Q2 builders
moved the main landing gear inboard. Even a brake on the
unloaded wheel
will not help.
I am sorry I did not think of that when you were building it Lewis.
All that beautiful rotary engine installation stuff you did was
just great.
Paul Lamar
Thanks for the kind words.
That was a rough day...
Still a huge fan of the engine. Despite the bitter ending, the
Cosmic Fish was a tremendous education.
The current conceptual airplane on my computer requires two rotary
engines. It's based a little on the vought flying pancake and some of
the bernelli designs. I'll fly a large scale model of it next year.
I've got a couple projects backlogged ahead of it, though
Lewis. Bjork
Do you have the classic book Theory of Wing Sections by Von Doenhoff?
Page 8 CsubD = CsubL squared divided by Pi times A
A is the aspect ratio or span divided by cord.
Very simple.
Bad aspect ratio bad MPG :-) The reason Lindberg got across the ocean
was he added wing span to the stock Ryan.
You can down load it here for free.
https://aeroknowledge77.files.wordpress.com/2011/09/58986488-theory-of-wing-sections-including-a-summary-of-airfoil-data.pdf
<https://aeroknowledge77.files.wordpress.com/2011/09/58986488-theory-of-wing-sections-including-a-summary-of-airfoil-data.pdf>
Or direct from the Publisher Dover. See attached.
Paul Lamar
Yes, I have that book.
Wing loading also plays a factor here. A light wing loading is how the
Duke Delta gets away with it's very low aspect ratio planform.
I'm hoping for structural efficiency and high AOA benefits in a compact
airplane.
There is argument whether the spiral airflow from the props actually
counters wing vortices as claimed with the vought design, but the
computer likes it, so far. That's why the model comes next.
Lewis. Bjork
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