Fred,
One doesn't have to pay for the "horsepower" gains from ram air, but I
agree with everything else, except your question.
Yes, if I were building today, the bottom of my cowl and airframe would
look a lot different. Cooling drag reduction thru augmentation with a benefit
from a wee bit of thrust to boot, ahhhh. Not to mention the ear splitting
addition of the noise to scare those on the ground and in the air.
I knew nothing when I started building last century - Now I know just
enough to get myself into trouble.
No, I am through experimenting with my flying lawn dart and its beautiful
cosmetics. Augmentation would require exhaust pipe and cowl modifications
at the very least. Then I would entrap myself with a cold induction
system. Arrrrggghh, it never ends.
We are all waiting for your computation-justifying flights. Alas, you are
not done just yet.
Scott
In a message dated 2/18/2008 1:47:04 P.M. Central Standard Time,
fredmoreno@optusnet.com.au writes:
“There
is a free lunch - or at least a cheap one.”
Right you are,
Scotty! I merely was pointing out that one has to pay for more
horsepower, or work for drag reductions.
However…..
There may be another
nearly free lunch. Exhaust thrust.
I have a WWII NACA
tech paper discussing the theoretical and experimental work done to determine
the potential thrust from the exhaust of aspirated piston engines. The
faster you go, the more effective it can be. So after evaluating all the
cooling drag reduction work I have done, I plan to work on this area next.
First I will have to
wade through all the equations and data and attempt to understand and
interpret it with my ever-shrinking neuronal capacity. That is a project for
the latter half of the year. Trading more back pressure (and presumably some
power loss) for thrust improvement (via exhaust nozzles) is an interesting
trade-off.
It is not a simple
one.
“Combining power
gains with drag reductions [and perhaps
some augmentation of exhaust thrust] results in
significantly greater performance.”
Want to try some
experiments?