Mailing List lml@lancaironline.net Message #41026
From: Walter Atkinson <walter@advancedpilot.com>
Sender: <marv@lancaironline.net>
Subject: Re: [LML] Re: Thielert Diesel Centurion 4.0
Date: Sun, 01 Apr 2007 12:09:20 -0400
To: <lml@lancaironline.net>
Ya think? <g>

The cooling drag increase can be in the 15-20% range.  Now, calculate the increased HP required to overcome that increase in drag.  It's not insignificant.  Were this simple to address the diesel aircraft would be faster and more efficient than they are.

Walter


On Mar 31, 2007, at 9:14 PM, REHBINC@aol.com wrote:

Scott,
 
Now that's what I like about the LML. I asked a question and in less than an hour someone provides an answer. Thanks.
 
So using this info in the previous scenario, a 10% change in cooling load would result in a 2% change in total drag. I like fast with payload, so I probably wouldn't be a diesel candidate. But 2% more drag is certainly not the end of the aviator's world. Even at full power a diesel is typically 3-5% more efficient than gas.
 
Rob




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