Return-Path: Received: from [24.25.9.103] (HELO ms-smtp-04-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.2b3) with ESMTP id 3221413 for flyrotary@lancaironline.net; Sat, 08 May 2004 08:35:26 -0400 Received: from EDWARD (clt25-78-058.carolina.rr.com [24.25.78.58]) by ms-smtp-04-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id i48CZNC9013339 for ; Sat, 8 May 2004 08:35:24 -0400 (EDT) Message-ID: <002b01c434f8$f2217830$2402a8c0@EDWARD> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Web hosting was : [FlyRotary] Re: Intake manifold tuning Date: Sat, 8 May 2004 08:35:28 -0400 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1409 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1409 X-Virus-Scanned: Symantec AntiVirus Scan Engine Good point, Eric I certain am not biased against Canards (even if they have the engine on the wrong end {:>)), I seriously considered a Long EZ but concluded that my flying needs (and reluctance to get into composite construction) dictated that the RV was the better aircraft for my purposes. I hesitate to post things that I have posted before so as not to unduly clutter up the list especially when they may be consider somewhat esoteric by most. I keep telling myself I should establish my own web site (my aircraft stuff is hosted on another individual's web site) to host such items. Right now I have several things that might be of interest. I have two spreadsheets that calculate power, fuel burn, rpm, BTU generated and some crude cooling models for both the NA and Turbo 13B which data has shown to have a fairly good correlation with what folks are reporting. I have over 18MB of presentation slides and "Formal" derivation of the Rotary Dynamic Intake Effect analysis. Its composed of 67 slides (PowerPoint) which is why its so large a file. Even zipped its 12 MB I have other bits and pieces from the Hemlhotz equation adapted for the rotary to cooling duct coordinate generators, to some early analysis of the cooling effectiveness of the Gm evaporator cores used by many. I hesitate to impose such a mess on anybody's web site. What I need to do it check with my Service Provider, they provide a 5 MB size web page hosting for free. I would need more than that, but it might be reasonable. Thanks for the suggestion about the Canard list. Ed Ed Anderson RV-6A N494BW Rotary Powered Matthews, NC ----- Original Message ----- From: "Eric Ruttan" To: "Rotary motors in aircraft" Sent: Saturday, May 08, 2004 12:42 AM Subject: [FlyRotary] Re: Intake manifold tuning > Ed; > I know you have posted this mathematical stuff before to this list, but > there are new members all the time, and some may not have been interested > when this was first posted, but they may have become more willing to follow > the math more closely. > > Might I suggest a posting of the relevant files to a web site. Easy to > reference and centralized , and the latest corrected version always > available are just a few advantages. > > I am sure there are a bunch of us capable of hosting these files, but I will > go further to suggest as forum such as > www.canardaviation.com/fourm > you could post the files in a thread there, or if you would prefer a new > forum could be created. It would be easy to reference and you can edit an > attached file to the latest version at any time. > > Please do not let the canard bias your decision. > We have no problem with those that choose to make their planes backward. :) > Again, any host will due. If I may be of assistance please ask. > Archive: http://lancaironline.net/lists/flyrotary/List.html >