Mailing List flyrotary@lancaironline.net Message #49941
From: MONTY ROBERTS <montyr2157@windstream.net>
Subject: Re: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo
Date: Tue, 9 Feb 2010 18:27:18 -0600
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Don't listen to whoever told you that George. It is application specific. You design it for what you are doing. Each design has an optimum point and it's worse everywhere else. All you can do is move it around.
 
I can't give specific advice...precisely because of all the variables. If you were paying me to design one, I would call Craig Catto. ;-)
 
Monty
----- Original Message -----
Sent: Tuesday, February 09, 2010 6:07 PM
Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo

Monty,
Prop efficiency climbs (so I'm told) until it reaches speed of sound, so I believe some try to take the prop  as close to 3,000 rpm as possible, yet some stay a conservative 2,700 rpm, what do you suggest, given all the variables.
George (down under)
 
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster