Return-Path: Received: from [65.33.164.27] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.1.4) with HTTP id 2602637 for lml@lancaironline.net; Wed, 24 Sep 2003 22:00:37 -0400 From: "Marvin Kaye" Subject: Re: [LML] Re: Gain a couple of knots To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.1.4 Date: Wed, 24 Sep 2003 22:00:37 -0400 Message-ID: In-Reply-To: <002501c38303$1fa8c2c0$0300a8c0@erics1200mhz> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Eric M. Jones" : Scott, It may well be that you are correct. I have done this in a C172 and the increase in speed is easily apparent (~2 knots). The rear CG condition leads to divergent pitch stability at low speeds. At cruise, you have lots to work with. A completely flying stab would be ideal for speed. >Bleriot never built a "high-performance" airplane. Oh really?......... >He didn't understand the drag reduction in laminar flow. They say the P51 wing was laminar flow. But good authority says it never was. There may not be such a thing. There is good flow and better flow, that's all. Regards, Eric