Mailing List flyrotary@lancaironline.net Message #28658
From: Bulent Aliev <atlasyts@bellsouth.net>
Subject: Re: [FlyRotary] Re: Props
Date: Wed, 21 Dec 2005 19:08:15 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
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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