Mailing List flyrotary@lancaironline.net Message #54786
From: Ernest Christley <echristley@att.net>
Subject: Re: [FlyRotary] Re: Cooling Inlets
Date: Sat, 30 Apr 2011 11:10:02 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Ed Anderson wrote:

For a high speed cruise environment, I would think cooling drag might be of more importance than say perhaps a few pounds of additional weight, on the other hand if you are flying an already draggy biplane for example, cooling drag is probably a very small part of your over all drag, but getting cooling with low airspeed might be the system driver.
 
Its all about compromises - space, weight, flow, drag, etc. - oh, yes! - and cooling of course {:>)  all matched to your constraints and operating environment.
 


I may have read it wrong, but it seems the NACA study that Tracy was referencing said that the cooling drag for the Aztec they were testing was about 5% to 7% of total drag.  I've read before that cooling drag is more like 30% of total drag.  Big difference there it seems.

Does anyone have any better insight, or is this just an apples vs oranges thing?  We've spent a LOT of time discussing cooling drag on this list.  Is it even worth worrying over?  Is it worth stressing over an engine overheating to go 196MPH instead of 192MPH?
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster