X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 20 May 2009 14:58:32 -0400 Message-ID: X-Original-Return-Path: Received: from n76a.bullet.mail.sp1.yahoo.com ([98.136.45.23] verified) by logan.com (CommuniGate Pro SMTP 5.2.14) with SMTP id 3647971 for lml@lancaironline.net; Wed, 20 May 2009 08:55:43 -0400 Received-SPF: none receiver=logan.com; client-ip=98.136.45.23; envelope-from=casey.gary@yahoo.com Received: from [69.147.84.144] by n76.bullet.mail.sp1.yahoo.com with NNFMP; 20 May 2009 12:55:07 -0000 Received: from [68.142.237.90] by t6.bullet.mail.sp1.yahoo.com with NNFMP; 20 May 2009 12:55:07 -0000 Received: from [69.147.75.190] by t6.bullet.re3.yahoo.com with NNFMP; 20 May 2009 12:55:07 -0000 Received: from [127.0.0.1] by omp106.mail.re1.yahoo.com with NNFMP; 20 May 2009 12:55:07 -0000 X-Yahoo-Newman-Property: ymail-5 X-Yahoo-Newman-Id: 199231.5128.bm@omp106.mail.re1.yahoo.com Received: (qmail 19050 invoked by uid 60001); 20 May 2009 12:55:05 -0000 DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=yahoo.com; h=Message-ID:X-YMail-OSG:Received:X-Mailer:References:Date:From:Subject:To:In-Reply-To:MIME-Version:Content-Type; b=MOOXJCdWJLxi6zecWmzJ3RUdeQ36TFp5OoFiea2mTxJF9hWp4zBqiDikGokOVjWIFOuoI8mVgdYttO7jgNkdRXUupG7NNQUyd1Z8OOlyDuY7IAcVH3ZzswGMBqQ+5KXx9bykaDGrcqEud1HaFyq/Eisg4414I+VOeI8GSNPnPoM=; X-Original-Message-ID: <362251.9407.qm@web57513.mail.re1.yahoo.com> X-YMail-OSG: D5jY2ccVM1mr.jCdPl7ltjP9iqFwaYeYKNG8g1jhTdsu0j2jbHAfR56KfN842ysBkCcRIFWZRziIMZr4Ke7JNbgFa3KoY9jr2j1D5vY9fNQl0Yv2aV_wEym1DMBme1AahGiV6cU.Uv5Hk5tjX8kQtYfsR6AUUe0lQajPue2zs5C2SwzEj_kfLHow068NPRdH8QuTLaCBK1XFIM5uV3AYL1TmQr04zuNIfqW8cemsuvaqud9mU4Ny86osLg_ybQMtJIEyOSfKfwey9vGTdmCRs3c2axSU7y4VR7wRtvkYXY6Eqt8ofs3BHvs9gIUPlh0bec8- Received: from [97.122.177.13] by web57513.mail.re1.yahoo.com via HTTP; Wed, 20 May 2009 05:55:04 PDT X-Mailer: YahooMailRC/1277.43 YahooMailWebService/0.7.289.10 References: X-Original-Date: Wed, 20 May 2009 05:55:04 -0700 (PDT) From: Gary Casey Subject: Re: Engine Out Practise(sic) X-Original-To: Lancair Mailing List In-Reply-To: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="0-1237312288-1242824104=:9407" --0-1237312288-1242824104=:9407 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable Grayhawk,=0AToo late {:-) I already looked at it. I compared it to the rou= gh formula I have always used - % power =3D RPM/RPMmax * MAP/MAPmax - and = it comes within 1% of it. I stopped there and didn't try to "reverse engin= eer" the formula, except I have hunch it has to do with assuming the max RP= M is 2500 (the 2.5) and the max MAP is 35 inches (the 3.5). Regardless, th= e formulas are not quite right. As rpm increases, engine friction increase= s and volumetric efficiency decreases so the increase in power won't go up = directly with RPM. The opposite is true of MAP. It takes a certain MAP ju= st to power the engine (overcome friction) so power will increase more than= the increase in MAP. How much are these effects? Without real data it wo= uld be hard to say, but in the RPM and MAP ranges that are useful in aircra= ft engines the factor for rpm might be something like 0.8. For MAP there is= a subtractive term of about 10 inches. The equation would then look like = %power =3D (RPM/RPMmax*0.8) * (MAP-10)/MAPmax-10). Gets hard to do in your head = (well, mine anyway), so I just remember that a 10% reduction in RPM will dr= op the power less than 10%, but a 10% drop in MAP will drop the power by mo= re than 10%. Then there is the effect of altitude..=0AGary=0A=0A=0A=0A____= ____________________________=0AFrom: Lancair Mailing List =0ASe=0A=0AIgnore the formula. I got it from a very old email and it= is=0Awrong. Perhaps Walter will correct it.=0A =0AGrayhawk the brainless= =0A =0AIn a message dated 5/18/2009 7:39:13 P.M. Central Daylight Time,=0AS= ky2high@aol.com writes:=0A =0AFinally, thanks to Walter at GAMI, =0A =0A%HP= =3D 100-((max RPM/100-RPM)*2.5+(Max MP-MP)*3.5)=0A=0A=0A --0-1237312288-1242824104=:9407 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
Grayhawk,
Too late {:-) I already looked= at it. =A0I compared it to the rough formula I have always used - % power = =3D RPM/RPMmax * MAP/MAPmax =A0- and it comes within 1% of it. =A0I stopped= there and didn't try to "reverse engineer" the formula, except I have hunc= h it has to do with assuming the max RPM is 2500 (the 2.5) and the max MAP = is 35 inches (the 3.5). =A0Regardless, the formulas are not quite right. = =A0As rpm increases, engine friction increases and volumetric efficiency de= creases so the increase in power won't go up directly with RPM. =A0The oppo= site is true of MAP. =A0It takes a certain MAP just to power the engine (ov= ercome friction) so power will increase more than the increase in MAP. =A0H= ow much are these effects? =A0Without real data it would be hard to say, bu= t in the RPM and MAP ranges that are useful in aircraft engines the factor for rpm = might be something like 0.8. For MAP there is a subtractive term of about 1= 0 inches. =A0The equation would then look like =A0%power =3D (RPM/RPMmax*0.= 8) * (MAP-10)/MAPmax-10). =A0Gets hard to do in your head (well, mine anywa= y), so I just remember that a 10% reduction in RPM will drop the power less= than 10%, but a 10% drop in MAP will drop the power by more than 10%. =A0T= hen there is the effect of altitude..
Gary


From: Lancair Mailing List <lml@lancaironline.net= >
Se


=0A= =0A =0A =0A=0A
Ignore the formula.=A0 I got it from a very old email and it= is=0Awrong.=A0 Perhaps Walter will correct it.
=0A
=A0
=0AGrayhawk the brainless
=0A
=A0
=0A
=0A
In a messag= e dated 5/18/2009 7:39:13 P.M. Central Daylight Time,=0ASky2high@aol.com wr= ites:
=0A
=0A
=A0
=0A
Finally= , thanks to Walter at GAMI,
=0A
=A0
=0A
%HP =3D 100-= ((max RPM/100-RPM)*2.5+(Max MP-MP)*3.5)
=0A
=A0


=0A=0A=0A=0A --0-1237312288-1242824104=:9407--