Mailing List flyrotary@lancaironline.net Message #58524
From: Richard Sohn <res12@fairpoint.net>
Subject: Re: [FlyRotary] Re: First lift off with single rotor
Date: Mon, 9 Jul 2012 12:05:52 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
I don’t consider cooling drag a significant issue on an airplane making barely 100MPH. The heat under the cowl is certainly something to be considered.
Thanks!!
 
Richard Sohn
N2071U

http://www.fairpoint.net/~res12/home.html
 
Sent: Monday, July 09, 2012 11:48 AM
Subject: [FlyRotary] Re: First lift off with single rotor
 
Congratulations Richard, it's a great start.
 
Big "general rule of thumb" is give your exit (in a low pressure area) 150% of air inlet area. Think of the impact heat has on air in a hot air balloon plus the under cowl turbulence and slowing the air way down in there it is easy to see back pressure building up.
It is a good starting point and you can always begin blocking off bits of both inlet and outlet once it all looks like it is cooling then you can begin working on lessening the cooling drag.
 
Chrissi & Randi

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In a message dated 7/9/2012 10:50:15 A.M. Central Daylight Time, res12@fairpoint.net writes:
Cleared the ground for a brief period today. As far as the airplane is concerned, everything is good. CG seems to be right on the spot. Much better as it was 12 years ago at the first flight with the SOOB.
Here is the reason why it was not a flight. A few days ago when I started high speed taxi, as soon as it picked up air speed, the engine started to sputter and almost cut out totally. This was at the same RPM as at a run up, where it does not do that. With a wiggly tail dragger as the Avid is, there was no way reading enough instrument for making a preliminary analysis. I recorded the instrument panel with a GoPro at 2sec intervals.
Looking at the first pictures, the answer came up right away, increasing pressure under the cowl where the intake for the engine is located. Like the EGT shot up over 1600 just before the sputtering started. Since my radiator air is going to the outside of the cowling, there was no impact on cooling. Btw cooling is really good. At an OAT of 95F, oil and water stayed at around 170F no matter what I did.
 
For todays runs, I taped the inlet around the prop hub shut. Sure enough, the sputtering occurred at higher airspeed, and was not as total, however, EGT was still going to around 1600.
 
The conclusion is, I have to open the cowling exits a lot.
 
Richard Sohn
N2071U

http://www.fairpoint.net/~res12/home.html
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