X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from poplet2.per.eftel.com ([203.24.100.45] verified) by logan.com (CommuniGate Pro SMTP 5.3.1) with ESMTP id 4095739 for flyrotary@lancaironline.net; Mon, 25 Jan 2010 19:11:06 -0500 Received-SPF: none receiver=logan.com; client-ip=203.24.100.45; envelope-from=lendich@aanet.com.au Received: from sv1-1.aanet.com.au (mail.aanet.com.au [203.24.100.34]) by poplet2.per.eftel.com (Postfix) with ESMTP id A5A6817389C for ; Tue, 26 Jan 2010 08:10:24 +0800 (WST) Received: from ownerf1fc517b8 (203.171.92.134.static.rev.aanet.com.au [203.171.92.134]) by sv1-1.aanet.com.au (Postfix) with SMTP id 7217ABEC019 for ; Tue, 26 Jan 2010 08:10:24 +0800 (WST) Message-ID: <44ED1E38721D4CEEA83E76A36A3B6788@ownerf1fc517b8> From: "George Lendich" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Wedge/Oblique Duct Date: Tue, 26 Jan 2010 10:10:25 +1000 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=response Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.5843 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5579 X-Antivirus: avast! (VPS 100125-2, 01/25/2010), Outbound message X-Antivirus-Status: Clean Ernest, You are most probably right, but I'm trying to think how the pros might do it on paper, before committing to a physical design. How might a Aeronautical Engineers tackle a problem like this - there are most probably some simple formulas, perhaps. George ( down under) > George Lendich wrote: >> Ed, >> I have been thinking about this, if I use A1V1=A2V2 to solve for the >> inlet opening size, how do I know if the speed of air through the duct is >> correct i.e. 10% for cruise and 30% for climb. >> Also If I use the Cessna 171 speed of approx 100 K for cruise = 10 K >> through core, 70 knot climb and approx 20 K through core. Do I then use >> the climb speed to calculate inlet air openings and attach an adjustable >> louver exit OR I suppose I could do as Tracy does and calculate for >> cruise and attach a spray bar. >> I'm still a little confused on the best approach. >> George ( down under) > George, maybe the problem is that there isn't a "best approach". There's > "not worth a cuss"; and there's "good enough". There might even be a > "works pretty dang good". Everybody wants bragging rights to having > landed the perfect solution on first flight, with the difference between > perfect and "get it in the air" being a few fpm in climb and a handful of > kts at cruise. > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html >