X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from fed1rmmtao103.cox.net ([68.230.241.43] verified) by logan.com (CommuniGate Pro SMTP 5.1.11) with ESMTP id 2241033 for flyrotary@lancaironline.net; Fri, 03 Aug 2007 19:34:57 -0400 Received-SPF: none receiver=logan.com; client-ip=68.230.241.43; envelope-from=alventures@cox.net Received: from fed1rmimpo01.cox.net ([70.169.32.71]) by fed1rmmtao103.cox.net (InterMail vM.7.08.02.01 201-2186-121-102-20070209) with ESMTP id <20070803233421.OZCS14885.fed1rmmtao103.cox.net@fed1rmimpo01.cox.net> for ; Fri, 3 Aug 2007 19:34:21 -0400 Received: from BigAl ([72.192.132.90]) by fed1rmimpo01.cox.net with bizsmtp id XbaK1X0081xAn3c0000000; Fri, 03 Aug 2007 19:34:19 -0400 From: "Al Gietzen" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] Re: Tips on tuning Date: Fri, 3 Aug 2007 16:36:29 -0800 Message-ID: <000001c7d62f$7fb19560$6400a8c0@BigAl> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.6626 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.3138 I'm all for 3 or more blades because there is more surface area to=20 impart thrust from. Since we have a prop disc limit of 66 inches on our=20 airframe, adding blades is the way to go to improve thrust. There is a=20 limit to the amount of HP a given blade can absorb and transmit. I=20 wouldnt necessarily be opposed to trying a 6 blade variant either,=20 provided we are making full power with our engine, or later with the = turbo. David; I'm quite certain it is not as simple as more blades equals more thrust. More blades equals more rotational drag, and each additional blade = getting a smaller "bite". If you are allowed the diameter needed to absorb the = power, two blades usually gives you the highest top speed. But a 3 blade is nice for a pusher; the general opinion is it is = smoother than 2 blades because both blades are not in the wing wake at the same = time. Al