Mailing List flyrotary@lancaironline.net Message #52516
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Fw: [FlyRotary] Effective Prop Pitch Calculations
Date: Sat, 9 Oct 2010 13:58:05 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>, Panzera Pat <editor.contactmagazine@gmail.com>
From Pat - appears my problem is not "slippage" but negative Thrust - well,  negative thrust does not sound very positive to me.  Now If I had it installed as a pusher prop would I pick up 4 MPH in airspeed - with the negative thrust now in the pushing direction {:>)
 
Ed

Sent: Saturday, October 09, 2010 1:45 PM
Subject: Re: [FlyRotary] Effective Prop Pitch Calculations

Please forward this thought for me:

No slippage, your root section is creating negative thrust since it's not pitched steep enough.



On Sat, Oct 9, 2010 at 10:16 AM, Ed Anderson <eanderson@carolina.rr.com> wrote:
I used the equation that Lipps mentions in the article in CONTACT! to Calculate "Effective Pitch" of my 74x88 prop.  His equation (with some clarifying annotations) is
 
Effective Pitch ( % ) = TAS (mph) *1056/RPM(Props' RPM not engine)
 
EF = 168*1056/2105 = 84.27 effective pitch
 
Since my Props pitch is suppose to be 88" could this mean I have a bit of "Slippage"?  Actually, I was impressed that the calculation came out as close as it did - within 4% of its 88" of pitch. 
 
Thanks Pat
 
Ed
 
 
Edward L. Anderson
Anderson Electronic Enterprises LLC
305 Reefton Road
Weddington, NC 28104
http://www.andersonee.com
http://www.eicommander.com

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