Return-Path: Received: from imo22.mx.aol.com ([198.81.17.66]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sat, 19 Jun 1999 15:26:14 -0400 Received: from Fredmoreno@aol.com (3956) by imo22.mx.aol.com (IMOv20) id kXBFa09518 for ; Sat, 19 Jun 1999 15:28:31 -0400 (EDT) From: Fredmoreno@aol.com Message-ID: <1496ebf0.249d495f@aol.com> Date: Sat, 19 Jun 1999 15:28:31 EDT Subject: Cooling a Walther turbine To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Let me know how much heat you want to dump (is there a figure in the engine spec?) and I can give it a crack. You can't get very much out of the wings because of the honeycomb/composite structure and the thick boundary layers compared to those in heat exchangers. You cannot get nearly enough heat to de-ice the wings. That takes lots of heat, more than composites can stand. (I examined running coolant from a liquid cooled engine in the leading edges. Forget it. Too many problems.) My initial guess is that you are much better off with the heat exchanger, but I would be happy to have a look and do a few calculations. Fred Moreno >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html