Mailing List lml@lancaironline.net Message #55236
From: Terrence O'Neill <troneill@charter.net>
Sender: <marv@lancaironline.net>
Subject: Re: [LML] Re: cowl flap cooling drag reduction
Date: Sun, 30 May 2010 01:09:28 -0400
To: <lml@lancaironline.net>
Thanks, Gary.  
Okay, so I think I would keep the L235 cowl inlet area as-is, and be generous with the flappable outlet area.
Actual experience is very reassuring.
Terrence
L235/320 N2111AL



 I also reduced the inlet area about 20%, adding a diffuser section.  The outlet area was reduced to about half of the original, depending on what kind of bulges on the bottom are assumed to be "standard."  The cooling is marginal, but adequate - on hot days climb speeds have to be increased and cruise is done with the flaps open.  This is to keep the CHT's below 400 and oil below 220.  Closing the relatively small cowl flaps increases the speed by 2 to 4 knots. 
ES #157, Lycoming engine
 

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