Mailing List flyrotary@lancaironline.net Message #28660
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: Props
Date: Wed, 21 Dec 2005 19:54:32 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Yes, George.  If we assumed no slip in the prop then theoretically the formula will give you the pitch of the prop you would need to screw through the air and achieve your MPH at your RPM input.  This is based simply on the screw principal.  I am certainly not a prop expert, but I also believe that since the prop is  a spinning wing (airfoil), that there is a lift component  in the direction of flight which may result in more speed than the formula could account for.  
 
Your second equation can be reduced further from   (Inches/Minute)/(RPM) = (Inches/Minute)/(Revs/Minute) = inches/Rev
 
Ed A
 
 
----- Original Message -----
Sent: Wednesday, December 21, 2005 7:08 PM
Subject: [FlyRotary] Re: Props

Don't ask me George. I'm not an engineer or good with mathematics. Ed A will know better.
Buly
On Dec 21, 2005, at 6:20 PM, george lendich wrote:

Thanks Buly,
So, Pitch"  = MPH x12 x 5280
                   RPM x 60
I figure 12 (inches in a foot) and 5280 ( feet in a mile) and 60 ( minute in an hour).
So the top line is converted into inches per minute and the bottom line RPM.
 
So, Pitch " = inches per minute
                    RPM
 
Does that look right to you ?
George ( down under)
 
 
Thanks George. my mistake was that i did not convert it to MPH.
I was also given the formula for cruise speed:

Pitch" x RPM x 60  = MPH
       12 x 5280

Buly
On Dec 21, 2005, at 4:39 PM, george lendich wrote:

Buly,
Looking at the formula given by members on this list, 2 out of 3 were spot
on with Hoverhawk and the third was close.

Examples:
1. Prop Dia x 3.1416x RPM/ 720 - Correct!

2. Prop RPM x Dia x .00436 - Correct ( 3.14/ 720 =.00436)

3. 3.14 x 64 {given prop dia} ( 5500/2.17 {given RPM})= 508346/707 -
slightly incorrect ( as compared to the other 3 examples, which include
Hoverhawk)

i.e 3.14/ 707 = .004809 whereas all the others are 3.14/ 720 = .00436.

Now that I have that sorted - can someone tell me how to calculate pitch,
easily!!
George ( down under)


Thanks Perry. This makes me feel much better. Looks like the formulas
given to me were not good.
Buly
On Dec 19, 2005, at 2:00 PM, Perry Casson wrote:

I think your math is off a bit - Here's a online calculator http://
www.hoverhawk.com/propspd.html

I think 6900 puts a 72" prop close to  mach 0.9 but I've never ran
mine above 6500

Perry Casson



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Buly




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