Mailing List flyrotary@lancaironline.net Message #6715
From: clive CLAPHAM <clive@clapham55.fsnet.co.uk>
Subject: Re: [FlyRotary] Re: Data? Was : Renesis & RD-1C drive testing
Date: Tue, 23 Mar 2004 08:13:18 -0000
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Hi
 
We found the same thing on Q2 vs Q235 the larger coarse prop had a lower drag than the small fine pitch.  The glide ratio with the Q235 is about 13:1 compared to a brick.  We have tried a constant speed on the Q2 and I was amazed at how much drag you could get when set max fine pitch.
 
P factor I suspect that the apparent surprise is to do with the reverse rotation of you former set up cancelling out some of the P factor (engine one way prop other way) so you mostly only have air flow related P factor.  Now you got engine+prop rotation+air flow to contend with. All good fun! 
 
Clive Clapham
 
Progress on direct drive 13B painfully slow.
----- Original Message -----
Sent: Monday, March 22, 2004 4:25 AM
Subject: [FlyRotary] Re: Data? Was : Renesis & RD-1C drive testing

 
 


> Most unexpected finding so far is the radically improved glide at idle
> setting.  Have no clue why.  Would have expected worse instead of better.

> Tracy

Don't you have radically increased pitch in the prop? That will do it.

Charlie

Yep, 88" pitch.  Guess I figured even at that blade angle air flow would be fully stalled past the prop and the disk area being larger would cause more drag.  I was obviously wrong. 

Also noticed that having a direct MPG readout makes finding the most efficient descent angle & throttle setting easy to find.  It's a lot different than on the other redrive/prop.

Tracy

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