X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from cdptpa-omtalb.mail.rr.com ([75.180.132.123] verified) by logan.com (CommuniGate Pro SMTP 5.3.10) with ESMTP id 4586405 for flyrotary@lancaironline.net; Sat, 20 Nov 2010 12:21:35 -0500 Received-SPF: pass receiver=logan.com; client-ip=75.180.132.123; envelope-from=eanderson@carolina.rr.com Return-Path: X-Authority-Analysis: v=1.1 cv=3jtQBdTzPyV+fq4oCU/u8ZPrJJGN11HvhaDVxyWhycI= c=1 sm=0 a=uD6Wf0l6qdcA:10 a=rPkcCx1H5rrOSfN0dPC7kw==:17 a=ayC55rCoAAAA:8 a=arxwEM4EAAAA:8 a=r1ClD_H3AAAA:8 a=7g1VtSJxAAAA:8 a=Ia-xEzejAAAA:8 a=T-hiUb2JhnuesAg_Zh0A:9 a=s7h80ihZMIOlK5blM2IA:7 a=JbJy_7x40yXC90Pg-HZgTadCZ6MA:4 a=wPNLvfGTeEIA:10 a=Qa1je4BO31QA:10 a=4bhaZh6xE-xCm0ej:21 a=rexqQeH47FaIKi8U:21 a=pGLkceISAAAA:8 a=wuSkdW2-7xvNYiaKRK0A:9 a=T2Gg9eIgwnVNC8m0E-0A:7 a=hqwufqvD6qdvZ-z7ykyExdIYaJkA:4 a=MSl-tDqOz04A:10 a=EzXvWhQp4_cA:10 a=f1kw_I4SOvUIruusXFcA:9 a=RF1I1zkauSRT-OkcwUuc3QP1uB8A:4 a=CsB7bOINMmgA:10 a=IXvauB37yLPwxe3B:21 a=MzpmWH9SoIRKKsDh:21 a=rPkcCx1H5rrOSfN0dPC7kw==:117 X-Cloudmark-Score: 0 X-Originating-IP: 174.110.167.5 Received: from [174.110.167.5] ([174.110.167.5:62782] helo=EdPC) by cdptpa-oedge02.mail.rr.com (envelope-from ) (ecelerity 2.2.3.46 r()) with ESMTP id E9/93-02631-B7308EC4; Sat, 20 Nov 2010 17:20:59 +0000 Message-ID: <502170BB5A2B4B36A441FB1D3ED16A35@EdPC> From: "Ed Anderson" To: "Rotary motors in aircraft" References: In-Reply-To: Subject: Re: [FlyRotary] Re: Exhaust Calcuations Date: Sat, 20 Nov 2010 12:20:40 -0500 MIME-Version: 1.0 Content-Type: multipart/mixed; boundary="----=_NextPart_000_002C_01CB88AD.584D45D0" X-Priority: 3 X-MSMail-Priority: Normal Importance: Normal X-Mailer: Microsoft Windows Live Mail 14.0.8117.416 X-MimeOLE: Produced By Microsoft MimeOLE V14.0.8117.416 This is a multi-part message in MIME format. ------=_NextPart_000_002C_01CB88AD.584D45D0 Content-Type: multipart/alternative; boundary="----=_NextPart_001_002D_01CB88AD.584D45D0" ------=_NextPart_001_002D_01CB88AD.584D45D0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Mark,=20 I did some algebraic manipulations to find HPL based on a selected HPD = (tube diameter) and got an answer. However, I am somewhat skeptical of = it although it does tend to fit with the general theory of larger dia = pipes =3D shorter lengths. By arbitrary selection an diameter - you automatically select the rpm = factor in the equation (but, its hidden in the HPD value). The way you = check what your new rpm sweet spot with the arbitrary diameter is to = vary the rpm in the first set of equations until you get the length = determined by manipulated equation. So the revised equation for 1.8" dia tubes gave 27.58" inches for the = HPL. You vary the rpm value in the first equations until you get an HPL = of 27.58" and you get an rpm of approx 7900 - so I agree, probably too = high for your configuration. Ed From: Mark Steitle=20 Sent: Saturday, November 20, 2010 11:18 AM To: Rotary motors in aircraft=20 Subject: [FlyRotary] Re: Exhaust Calcuations Ed,=20 OK, that answers my question. By going with 1-7/8" OD pipe (.049 wall), = it would be tuned for about 7800 rpm. Obviously, this is too high for = our purposes. I'll go with 1-5/8 (.063 wall) to shoot for 6700 rpm peak = power. This is typically the rpm I see on ground roll and early climb = before I start adjusting the prop down to a lower rpm to transition to = cruise climb.=20 Have you used the header designer tool available from Burns Stainless? = You need to know all the timing numbers, rpm, etc. I may give it a try = and see what I come up with. I have a test p-port housing that I made = up to see if the tube could be welded to the inner liner. So, I can use = that with a spare rotor to verify the EVO and EVC numbers. =20 Mark On Sat, Nov 20, 2010 at 9:55 AM, Ed Anderson = wrote: Mark,=20 Here is the corrected spreadsheet - I've colored the changeable cells = blue - you can plug in any rpm and EVO. The rest of the cells are = protected to keep from accidently overwriting them. Ed Edward L. Anderson Anderson Electronic Enterprises LLC 305 Reefton Road Weddington, NC 28104 http://www.andersonee.com http://www.eicommander.com -- Homepage: http://www.flyrotary.com/ Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html ------=_NextPart_001_002D_01CB88AD.584D45D0 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Mark,
 
I did some algebraic manipulations to find HPL = based on a=20 selected HPD (tube diameter) and got an answer.   However, I = am=20 somewhat skeptical of it although it does tend to fit with the general = theory of=20 larger dia pipes =3D shorter lengths.
 
By arbitrary selection an diameter  - you=20 automatically select  the rpm factor in the equation (but, its = hidden=20 in the HPD value).  The way you check what your new rpm sweet = spot =20 with the arbitrary diameter is to vary the rpm in the first set of = equations=20 until you get the length determined by manipulated = equation.
 
So the revised equation for 1.8" dia tubes gave = 27.58"=20 inches for the HPL.  You vary the rpm value in the first equations = until=20 you get an HPL of 27.58" and you get an rpm of approx 7900 - so I agree, = probably too high for your configuration.
 
Ed
 
From: Mark Steitle
Sent: Saturday, November 20, 2010 11:18 AM
To: Rotary motors in = aircraft
Subject: [FlyRotary] Re: Exhaust = Calcuations

Ed,=20

OK, that answers my question.  By going with 1-7/8" OD pipe = (.049=20 wall), it would be tuned for about 7800 rpm.  Obviously, this is = too high=20 for our purposes.  I'll go with 1-5/8 (.063 wall) to shoot for 6700 = rpm=20 peak power.  This is typically the rpm I see on ground roll and = early climb=20 before I start adjusting the prop down to a lower rpm to transition to = cruise=20 climb.=20

Have you used the header designer tool available from Burns = Stainless?=20  You need to know all the timing numbers, rpm, etc.  I may = give it a=20 try and see what I come up with.  I have a test p-port housing that = I made=20 up to see if the tube could be welded to the inner liner.  So, I = can use=20 that with a spare rotor to verify the EVO and EVC numbers.  
 
Mark


On Sat, Nov 20, 2010 at 9:55 AM, Ed Anderson = <eanderson@carolina.rr.com&g= t;=20 wrote:
Mark,
 
Here is the corrected spreadsheet - I've = colored the=20 changeable cells blue - you can plug in any rpm and EVO.  The = rest of the=20 cells are protected to keep from accidently overwriting = them.
 
Ed
 
Edward L. Anderson
Anderson Electronic = Enterprises=20 LLC
305 Reefton Road
Weddington, NC 28104
http://www.andersonee.com
http://www.eicommander.com

= --
Homepage:=20  http://www.flyrotary.com/
Archive and UnSub: =   http://mail.lancaironline.net:81/lists/flyrotary/List.htm= l


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