X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 20 Feb 2008 15:20:13 -0500 Message-ID: X-Original-Return-Path: Received: from smtp.perigee.net ([206.229.254.14] verified) by logan.com (CommuniGate Pro SMTP 5.2.0) with ESMTPS id 2737358 for lml@lancaironline.net; Tue, 19 Feb 2008 17:29:34 -0500 Received-SPF: none receiver=logan.com; client-ip=206.229.254.14; envelope-from=jschroeder@perigee.net Received: from john-study-2 (dsl-208-26-41-175.perigee.net [208.26.41.175]) by smtp.perigee.net (8.14.1/8.14.1) with ESMTP id m1JMSnqM008175 for ; Tue, 19 Feb 2008 17:28:50 -0500 X-Original-To: "Lancair Mailing List" Subject: Re: [LML] Re: Cold Induction, Power, and Speed References: X-Original-Message-ID: X-Original-Date: Tue, 19 Feb 2008 17:28:43 -0500 From: "John Schroeder" Content-Type: text/plain; format=flowed; delsp=yes; charset=utf-8 MIME-Version: 1.0 Content-Transfer-Encoding: 8bit In-Reply-To: User-Agent: Opera M2/8.54 (Win32, build 7730) Fred - On the old navigation trainers (T-29A, B, and C models) the Air Force had an augmenter tube into which they dumped the exhaust from the R2800 engine - one on each wing. It worked well and also was a source for hot air to deice the leading edges of the wing and horizontal stab. The Airline versions were Convair 330 and 440, I believe, and i don't know if they had that installation. Now that dates me for the world!! Scott - This installation had a very nice, throaty roar to it Not too loud. John Schroeder LNCE >Yes, if I were building today, the bottom of my cowl and airframe would look > a lot different. Cooling drag reduction thru augmentation with a benefit > from a wee bit of thrust to boot, ahhhh. Not to mention the ear splitting > addition of the noise to scare those on the ground and in the air. > >In a message dated 2/18/2008 1:47:04 P.M. Central Standard Time, > fredmoreno@optusnet.com.au writes: > > “There is a free lunch - or at least a cheap one.” > Right you are, Scotty! I merely was pointing out that one has to pay for > more horsepower, or work for drag reductions. > However….. > There may be another nearly free lunch. Exhaust thrust. > I have a WWII NACA tech paper discussing the theoretical and experimental > work done to determine the potential thrust from the exhaust of aspirated > piston engines. The faster you go, the more effective it can be. So after > evaluating all the cooling drag reduction work I have done, I plan to work on this > area next. > First I will have to wade through all the equations and data and attempt to > understand and interpret it with my ever-shrinking neuronal capacity. That is > a project for the latter half of the year. Trading more back pressure (and > presumably some power loss) for thrust improvement (via exhaust nozzles) is an > interesting trade-off. > It is not a simple one. > “Combining power gains with drag reductions [and perhaps some augmentation > of exhaust thrust] results in significantly greater performance.” > Want to try some experiments? > > > > > **************Ideas to please picky eaters. Watch video on AOL Living. > (http://living.aol.com/video/how-to-please-your-picky-eater/rachel-campos-duffy/ > 2050827?NCID=aolcmp00300000002598) >