X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from fmailhost02.isp.att.net ([207.115.11.52] verified) by logan.com (CommuniGate Pro SMTP 5.3.3) with ESMTP id 4152523 for flyrotary@lancaironline.net; Thu, 04 Mar 2010 15:54:18 -0500 Received-SPF: none receiver=logan.com; client-ip=207.115.11.52; envelope-from=bbradburry@bellsouth.net Received: from desktop (adsl-230-67-114.mco.bellsouth.net[74.230.67.114]) by isp.att.net (frfwmhc02) with SMTP id <20100304205343H0200nrfu9e>; Thu, 4 Mar 2010 20:53:43 +0000 X-Originating-IP: [74.230.67.114] From: "Bill Bradburry" To: "'Rotary motors in aircraft'" References: In-Reply-To: Subject: RE: [FlyRotary] Re: Vance Jaqua and Propellers Date: Thu, 4 Mar 2010 15:53:44 -0500 Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Mailer: Microsoft Office Outlook 11 Thread-Index: Acq72VdGlhA89qmHSJKc8Eh09rDJ5AAApxwA X-MimeOLE: Produced By Microsoft MimeOLE V6.0.6001.18049 Bryan, The AoA will decrease as the prop is moved thru the air in a forward direction. This may be a little difficult to visualize but think what would happen if the plane was moving forward and the prop was not rotating. The air hitting the front of the blade would have to do something to get around the prop blade. Some of it would flow across the top of the blade and some of it would roll around the leading edge and flow across the bottom of the blade. This would produce a flow of air that was oriented to the direction the blade would be moving if it were rotating. This same flow happens when the blade IS rotating and the plane is moving forward. This is what causes the AoA to be reduced. Bill B -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Bryan Winberry Sent: Thursday, March 04, 2010 3:28 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Vance Jaqua and Propellers Thanks Ernest, Can you splain me one thin. How does the AoA change on a fixed pitch prop? Bryan Disregard previous empty reply -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Ernest Christley Sent: Thursday, March 04, 2010 3:01 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Vance Jaqua and Propellers Bryan Winberry wrote: > > Ed, > > You're losing me here. If I understand you correctly, you are taking > off with lower prop RPM now compared to the original prop? But the > RD-1C allows the engine to produce more HP(via more rpm). Isn't the > goal to turn the prop just short of its' max RPM for T/O? Come to > think of it, maybe that's your point. Do you know the prop rpm's for > the two scenario's? > > Bryan > Bryan, wouldn't it be great if you were only trying to optimize two variables. Hp is tied to RPM. The faster you turn, the more Hp you get. The more Hp you get, the faster you turn. Blade pitch is tied to AoA (angle of attack). Add more pitch, the blade has higher AoA and tries to gulp more air. AoA is tied to RPM. Take little bites of air, and you can take them faster. Try to take to big of a bite, and you don't get any (the blade stalls). Blade length is tied to Hp. It takes power to move that cylinder of air. The bigger the cylinder, the more power required. dV (acceleration of the air) is tied to AoA. If you're taking bigger bites, the air has to move through faster. AoA is tied to the airplane's speed. As the plane accelerates, the prop blades AoA flattens out. Now, let's go through the optimized blade design process. You want a climb prop. You want maximum Hp right off the line, so pick a high RPM for the static tests. Pick the longest blade that will fit on your plane, and pitch it to absorb that Hp that is produced at that RPM. Now the blade will have much to little AoA at the chosen cruise RPM and speed. So, you shorten the blade and increase the pitch. You end up absorbing the same Hp, but the second blade absorbs more at a faster speed. You want a cruise prop. Maybe start with the target RPM for the engine on the takeoff role. This will translate to a certain Hp, that goes through your reduction gear of choice to give a prop RPM. I would pick a blade pitch such that the prop would be just barely past stalled. I would know this, because using a short field technique I would apply full breaks at the end of the runway until the engine came up to speed. When the ASI comes alive I'll note that the the RPM begins to drop off a little (the forward speed drops the blades AoA lets it move out of stall). At cruise speed, the blade will be in a drag bucket (most efficient) at my cruise RPM. I'll modify the blade length to absorb whatever Hp the engine is producing at takeoff. If you follow this thought process for real, and bolt the result to the front of your real plane, it might be the last thing you do. If you spend $50 on a copy of Xplane, you can play with it all day long (minus potty breaks) to see the effects. In any case, there isn't *A* goal. There are a bunch of goal*S*, with each one starting from a slightly different initial set of circumstances. I think someone smart once said, "It depends." 8*) -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html