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How do you download it? All I get is the
cover???
Bill B
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Ed Anderson
Sent: Saturday, October 09, 2010
12:40 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Fw:
[FlyRotary] Re: Propeller design.
Pat, asked to post this to the list - another Lipps article
in CONTACT!
I'm going there to read it now
Sent: Saturday,
October 09, 2010 12:19 PM
Subject: Re:
[FlyRotary] Re: Propeller design.
Ed,
I can't post to the group so could you please let everyone know that
the current issue of CONTACT! Magazine has another Lipps article in it and the
entire issue can be downloaded for free off the website. www.ContactMagazine,com
Pat
On Sat, Oct 9, 2010 at 7:23 AM, Ed Anderson <eanderson@carolina.rr.com>
wrote:
Yes, a radially different concept for
Prop design. I remember when the bi-plane picked up something like a 20
MPH increase in speed with Lipps prop - it had us all drooling to think that
perhaps we could gain a 10 MPH increase with our RV aircraft.
Unfortunately, in the one example I am somewhat familiar with when put on an
Rv-6 the outcome was somewhat disappointing - I think it was a gain of only
about 1-2 MPH.
Now in all fairness, Paul's admits
his design approach is dependent on somewhat untradiational accuracy in
engine HP and drag of the platform information - which may have been lacking in
this first attempt. However, since there has not been a flood of aircraft
with the Lipps prop, I'm inclined to believe that it has not yet reach the
promise that first seemed likely.
While folks can point to the 20 mph
increase in the bi plane's performance, I can't help but wonder if perhaps the
original prop on the bi plane may have been a poor choice whereupon replacing
it with the Lipps (better matched) make the performance gain seem all related
to the Lipps prop rather than replacing what may have been a poor original
choice - but, just spectulation on my part.
I really wanted to see the Lipps prop
deliver all it initially seemed to promise, but I can't find any data yet to
support its initial promise - at least on the type platforms and speeds we
normally fly. It’s the first really different approach to prop design
I've seen since - well, since the Wright brothers {:>)
If anybody has a source for information
that indicates my impression is incorrect regarding its performance on Rv type
aircraft (or similar), I would like to receive it.
Sent: Saturday, October 09,
2010 9:53 AM
Subject:
[FlyRotary] Propeller design.
I sat through a talk by Paul Lipps at
Gene Nevada at the alternative engine seminar put on by Contact Magazine
several years ago.
He flew in his home built, with his
propeller. Its outer blades were the size of a 12" ruler. Imagine model
sail plane wings, or bread knife blades. He placed split tennis balls on the
tips so guests did not stab themselves on the blades.
Later, he helped a guy design new wings
for a biplane racer, and those wings looked just like his propeller
blades. It had a 4 bladed Lipps propeller
as well.
Not mentioned was the low wetted area of the
blades would allow greater span with less drag. The high angle of attack at the
root allowed playing card sized cooling inlets.
In the event of failed engine his prop
has less than a 3rd of the frontal area of a conventional prop.
Not exactly full feathering, but better
than anything else.
So, if the blade has less drag for each
unit of lift, then you could add span until you get close to the ground, and
then add blade count until you have accounted for all of the available HP. Then
you port the rotary to get more HP.
Warning, looking at a Lipps propeller
blade may hurt your mind......................
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