Return-Path: Received: from [24.25.9.103] (HELO ms-smtp-04-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.2b2) with ESMTP id 3183503 for flyrotary@lancaironline.net; Wed, 21 Apr 2004 21:35:45 -0400 Received: from nc.rr.com (cpe-024-211-178-221.nc.rr.com [24.211.178.221]) by ms-smtp-04-eri0.southeast.rr.com (8.12.10/8.12.7) with ESMTP id i3M1ZhC8002439 for ; Wed, 21 Apr 2004 21:35:44 -0400 (EDT) Message-ID: <40871CE5.3050702@nc.rr.com> Date: Wed, 21 Apr 2004 21:16:21 -0400 From: Ernest Christley User-Agent: Mozilla/5.0 (X11; U; Linux i686; en-US; rv:1.6) Gecko/20040113 X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Performance Props References: In-Reply-To: Content-Type: text/plain; charset=us-ascii; format=flowed Content-Transfer-Encoding: 7bit X-Virus-Scanned: Symantec AntiVirus Scan Engine Perry Mick wrote: > On Wed, 21 Apr 2004 21:11:20 -0400, Chad Robinson wrote > >>Perry, if you could share the formulae you're using I'd be happy to >>make a spreadsheet calculator for this. So far I've found very >>complex prop calculators but nothing straightforward. >> >>By the way, why are you asking desired cruise speed? 400 knots! =) >> >>Do your calculations focus on pitch/length or do they also provide >>some means of calculating dimensions at various stations from the >>hub, so forming templates can be made? >> >>Regards, >>Chad >> > > It's not simple enough to put in a spreadsheet. > I think Al Wick uses the Bates Prop program, I don't know anything about > that program and I don't know why he couldn't develop numbers for Bulent. > The programs I use are all in the book "Modern Propeller and Duct Design" by > Martin Hollman. They are BASIC programs that I have improved on and now run > as visual basic macros. They have proven to be very good at predicting > reality. > Data entry is actual blade parameters along the length of the blade, so the > process is "trial-and-error". Enter a blade design and examine the output to > see what the performance is. The Bates program might be the opposite, enter > performance numbers and it spits out a blade design (?). > I want to know desired cruise speed and cruise RPM as a first estimate for > pitch. Actual cruise speed is limited by thrust produced and the drag of the > airplane, so equivalent flat plate area of the airplane is also a desirable > thing to know. > > Perry > Perry, would you like to share your algorithms. I'll turn them into C code ('cause I like C), and put a genetic algorithm on the front end. I'm assuming you have X number of stations that you enter numbers for. Make each station a genetic marker, start with a couple strains and let them mate through a few thousand generations till you get something you really like. -- http://www.ernest.isa-geek.org/ "Ignorance is mankinds normal state, alleviated by information and experience." Veeduber