X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from cdptpa-omtalb.mail.rr.com ([75.180.132.123] verified) by logan.com (CommuniGate Pro SMTP 5.2.8) with ESMTP id 3213342 for flyrotary@lancaironline.net; Tue, 14 Oct 2008 22:20:12 -0400 Received-SPF: pass receiver=logan.com; client-ip=75.180.132.123; envelope-from=echristley@nc.rr.com Received: from [192.168.0.19] (really [66.57.38.121]) by cdptpa-omta06.mail.rr.com with ESMTP id <20081015021936.CJQU18245.cdptpa-omta06.mail.rr.com@[192.168.0.19]> for ; Wed, 15 Oct 2008 02:19:36 +0000 Message-ID: <48F553EF.6080708@nc.rr.com> Date: Tue, 14 Oct 2008 22:22:39 -0400 From: Ernest Christley User-Agent: Thunderbird 2.0.0.16 (X11/20080724) MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: [Fwd: Cost Powercore Welding] References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit George Lendich wrote: > Ernest, > I agree it is interesting; my concern is that the wing tanks are > separated by wing ribs with only a small flapped opening between each, > this would require a lot of joins and odd shaped individual cells. > > This could however be used for some behind the spar tanks to increase > capacity and endurance, where space was available OR extra capacity in > the fuselage etc. Weight and balances concerns aside. > George (down under) George, I'm always biased, and don't understand you builders with your skinny wing 8*) The Delta has over 18 inches of depth at the strake, so one bay on each side is plenty enough if one chose to relocate the fuel tank. I didn't realize that the tanks were split up like that in skinny winged planes. -- http://www.ernest.isa-geek.org