Mailing List flyrotary@lancaironline.net Message #49954
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: RE: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo
Date: Wed, 10 Feb 2010 07:57:16 -0500
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>

Well, I claimed 4 MPH more on the top end, but what the heck it might have been 5-6 kts, I just wasn’t interested in that end of the performance spectrum to pay a lot of attention nor attempt to nail it down..

 

Ed

 


From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Al Gietzen
Sent: Tuesday, February 09, 2010 6:47 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo

 

Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo

 

Hp = C*V^3

 

Is that simple enough?

Simple enough – and with some other numbers Ed gave I compute he should get 5-6 kts more top end.

Al



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