X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail-bw0-f226.google.com ([209.85.218.226] verified) by logan.com (CommuniGate Pro SMTP 5.3.2) with ESMTP id 4118490 for flyrotary@lancaironline.net; Tue, 09 Feb 2010 19:45:31 -0500 Received-SPF: pass receiver=logan.com; client-ip=209.85.218.226; envelope-from=lehanover@gmail.com Received: by bwz26 with SMTP id 26so643033bwz.7 for ; Tue, 09 Feb 2010 16:44:56 -0800 (PST) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=gamma; h=domainkey-signature:mime-version:received:date:message-id:subject :from:to:content-type; bh=fCKaHRLPDfTtIG6dcvd5JzWy2gjsw1nCVPD2NFAtECs=; b=HKban4rsrni1wSj8ilz/hQrhfxAdIgLFqGwctCCYwn59+pDPOA/b4T3nuueRZIgx/v 198BahyJXSNijFXYPy4OTtQOLEwmAYG7qrznChI61K2m4FxEfjrNQWHxprIWDmsLcvQJ 6FCzIdDigqQJD1XIzOmmIbSNtHvEARTmT/BeU= DomainKey-Signature: a=rsa-sha1; c=nofws; d=gmail.com; s=gamma; h=mime-version:date:message-id:subject:from:to:content-type; b=i8DdT7mq6DvW7K5Rlr+Hpd4UyUfbh9o3BtwTB4St+FCztzVMc+GE6xo8ltNLYShWqL fQzDfnw7T15/hijxHFPM0jy0Zoagn1lEOZbKEJM4q90UXnOW/HHoFqzjxYa2Y39lnFfs azxShb7o55ZcZ02nCc2DCtfE3iS6vZ/cOl/cw= MIME-Version: 1.0 Received: by 10.204.3.207 with SMTP id 15mr1964146bko.91.1265762692861; Tue, 09 Feb 2010 16:44:52 -0800 (PST) Date: Tue, 9 Feb 2010 19:44:52 -0500 Message-ID: <1ab24f411002091644x3ba834dawb02eaa624b7689ce@mail.gmail.com> Subject: Less power, more speed. From: Lynn Hanover To: flyrotary@lancaironline.net Content-Type: multipart/alternative; boundary=000e0cd1e218ad8e45047f3457a8 --000e0cd1e218ad8e45047f3457a8 Content-Type: text/plain; charset=ISO-8859-1 Prop efficiency climbs (so I'm told) until it reaches speed of sound, so I believe some try to take the prop as close to 3,000 rpm as possible, yet some stay a conservative 2,700 rpm, what do you suggest, given all the variables. George (down under) Calculating the propeller tip speed just gets you close, because the airflow over the forward side of the blade reaches supersonic before the blade speed. The spreadsheets for calculating all of this neat airplane stuff (by John Roncz) are available on the EAA web page. If you have no spreadsheet, you can download one from Open Office.org for free. Or the whole office suite. Works great. Compatible with everything, free. You can fill in the dimensions of your plane and prop data and crank out the actual performance data within a percent or so. Scary accurate. Lynn E. Hanover --000e0cd1e218ad8e45047f3457a8 Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable
Prop efficiency climbs (so I'm tol= d) until it reaches speed of sound, so I believe some try to take the prop= =A0 as close to 3,000 rpm as possible, yet some stay a conservative 2,700 r= pm, what do you suggest, given all the variables.
George (down under)
=A0
Calculating the propeller tip speed just gets you close, because the a= irflow over the forward side of the blade reaches supersonic before the bla= de speed.
=A0
The spreadsheets for calculating all of this neat airplane stuff (by J= ohn Roncz) are available on the EAA web page.
=A0
=A0
If you have no spreadsheet, you can download one from Open Office.org<= /div>
=A0for free. Or the whole office suite. Works great. Compatible with e= verything, free.
=A0
You can fill in the dimensions of your plane and prop data and crank o= ut the actual performance data within a percent or so. Scary accurate.
=A0
Lynn E. Hanover
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