Return-Path: Received: from relay01.roc.ny.frontiernet.net ([66.133.182.164] verified) by logan.com (CommuniGate Pro SMTP 4.3c1) with ESMTP id 743913 for flyrotary@lancaironline.net; Fri, 18 Feb 2005 00:15:41 -0500 Received-SPF: pass receiver=logan.com; client-ip=66.133.182.164; envelope-from=canarder@frontiernet.net Received: from filter03.roc.ny.frontiernet.net (filter03.roc.ny.frontiernet.net [66.133.183.70]) by relay01.roc.ny.frontiernet.net (Postfix) with ESMTP id B8DBF364E30 for ; Fri, 18 Feb 2005 05:14:56 +0000 (UTC) Received: from relay01.roc.ny.frontiernet.net ([66.133.182.164]) by filter03.roc.ny.frontiernet.net (filter03.roc.ny.frontiernet.net [66.133.183.70]) (amavisd-new, port 10024) with LMTP id 18406-13-74 for ; Fri, 18 Feb 2005 05:14:56 +0000 (UTC) Received: from [127.0.0.1] (67-137-75-55.dsl2.cok.tn.frontiernet.net [67.137.75.55]) by relay01.roc.ny.frontiernet.net (Postfix) with ESMTP id 17A73364AB2 for ; Fri, 18 Feb 2005 05:14:55 +0000 (UTC) Message-ID: <421579C6.8040905@frontiernet.net> Date: Thu, 17 Feb 2005 23:14:46 -0600 From: Jim Sower User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.7) Gecko/20040514 X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: I found the power References: In-Reply-To: Content-Type: text/plain; charset=us-ascii; format=flowed Content-Transfer-Encoding: 7bit X-Antivirus: avast! (VPS 0507-3, 02/17/2005), Outbound message X-Antivirus-Status: Clean X-Virus-Scanned: by amavisd-new-20040701 (2.0) at filter03.roc.ny.frontiernet.net And just how might you massage those numbers to adapt them to a pusher? David Carter wrote: >Rather than NACA, might consider a "speed mod" described in book "Speed with >Economy" by Kent Paser, Paser Publications, 5672 West Chesnut Ave, >Littleton, Colorado 80123 (1994), Chapter 3, Engine Intake System >Modifications, starting page 52, ". . . use of propellor pressure pulses to >augment the ram air flow into the cowl carb air scoop." . . . ". . .the >scoop was extended forward about 8 inches, and the scoop opening was >rounded-off with an inlet area reduced to about 1.5 times that required for >sufficient flow to the carburetor. . . the scoop clears the propellor by >only 5/8 of an inch, with an inlet area only 10% larger than the venturi >throat area of the carburetor. . . .The scoop inlet is . . .about a 10 >degree angle into the advancing propellor blade. . .the sides of this inner >liner diverge at less than an 11 degree total angle. Any larger . . .and >the scoop would go turbulent" > >David Carter > > > > >