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Yep, if my HP calculations are correct and my aircraft weights what I think
it does, I should pick up 600 fpm rate of climb just on the HP. Correlates
with your 22 fpm/hp.
Ed
Ed Anderson
RV-6A N494BW Rotary Powered
Matthews, NC
----- Original Message ----- From: "Charlie England" <ceengland@bellsouth.net>
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: Wednesday, July 21, 2004 6:23 PM
Subject: [FlyRotary] Re: Tracy Report
Russell Duffy wrote:
> Since Tracy and I had the same static rpm with the previous props
> (which were the same made by Performance Prop), I expect I would have
> the same static he is getting if I had the 74" which I believe he
> indicated was around 6200 rpm or about 1000 rpm higher than with the
> old 2.14 and 68x72" prop. That 1000 rpm increase will translate into
> approx 30HP more for take off and move the torque from 345 lb-ft to
> 455 lb-ft or a gain of approx 110 lb-ft torque for take off.
> According to my spreadsheet that would move the take off HP from
> around 155 up to 185 for a standard day - in the cooler weather of
> all, it will be even more impressive.
>
>
> Talking to Tracy about the difference between his B and C setups got
> me all excited again. Sounds like he was REALLY happy with the
> performance difference.
>
> There's a fairly simple formula I saw once that converts excess HP to
> climb rate, given the weight of the plane. Do you have that? It
> would be interesting to see what 30 extra HP would do.
>
> Cheers,
> Rusty (I need a runway)
1hp=33,000 lb raised 1 foot per minute
A rough number should be 33000/gross weight * excess hp.
@ 1500 lb, 22 fpm per hp, minus small compensation for drag due to
increased angle of attack.
Does that pass a sanity check?
Charlie
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