X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.2 cv=cojZqBwi c=1 sm=1 tr=0 a=ZEnJ6fiDd6jScfGCWwM2RA==:117 a=wdrU7cV_hWgA:10 a=sSUyiyhxLBkA:10 a=x7bEGLp0ZPQA:10 a=Fee85h93u3AA:10 a=ocR9PWop10UA:10 a=Ia-xEzejAAAA:8 a=pGLkceISAAAA:8 a=7g1VtSJxAAAA:8 a=2tnqAtAMztdJVL2q610A:9 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=mDELarejG2Ns1rE4fHAA:9 a=iTgNUIdTRWpBb_VP:21 a=_W_S_7VecoQA:10 a=Urk15JJjZg1Xo0ryW_k8:22 a=grOzbf7U_OpcSX4AJOnl:22 From: " Lehanover@aol.com" Received: from omr-a008e.mx.aol.com ([204.29.186.51] verified) by logan.com (CommuniGate Pro SMTP 6.2.0) with ESMTPS id 10483752 for flyrotary@lancaironline.net; Thu, 28 Dec 2017 21:07:56 -0500 Received-SPF: pass receiver=logan.com; client-ip=204.29.186.51; envelope-from=Lehanover@aol.com Received: from mtaomg-aaj02.mx.aol.com (mtaomg-aaj02.mx.aol.com [172.27.3.208]) by omr-a008e.mx.aol.com (Outbound Mail Relay) with ESMTP id 67FFF3800083 for ; Thu, 28 Dec 2017 21:07:40 -0500 (EST) Received: from core-mda04d.mail.aol.com (core-mda04.mail.aol.com [172.27.39.4]) by mtaomg-aaj02.mx.aol.com (OMAG/Core Interface) with ESMTP id 2057F38000085 for ; Thu, 28 Dec 2017 21:07:39 -0500 (EST) Full-name: Lehanover Message-ID: Date: Thu, 28 Dec 2017 21:07:39 -0500 Subject: Re: [FlyRotary] Re: Cooling Issues To: flyrotary@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="part1_c718c.5244be7a.4776fd6a_boundary" X-Mailer: AOL 9.8 sub 2024 X-Originating-IP: [24.164.30.24] x-aol-global-disposition: G DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=mx.aol.com; s=20150623; t=1514513260; bh=mGGDVe1dTIFLvjiyy5crMSSAp+EaW0Cf+98emdGKA2Y=; h=From:To:Subject:Message-ID:Date:MIME-Version:Content-Type; b=TkZC1Jz4vrCM3wTS/85oI8LzVZNILeRVOP0QHdAZTyr96v5SmT2CZ76bPWWrxjXQ+ 6UWorr689m+6MNYjhS5/3lnarVnSEq/rcmWHtQ+JSyNGfrwapAZMHBWEsLu4WoLkvx uWPbH59W65VZMHGQhqkSSDeyUcL16tX2iuvRN1kU= x-aol-sid: 3039ac1b03d05a45a36b3b18 --part1_c718c.5244be7a.4776fd6a_boundary Content-Type: text/plain; charset="UTF-8" Content-Transfer-Encoding: quoted-printable Content-Language: en Are these cooling tests being done at speed, say 60 to 70 MPH? Or, =20 stationary? It only needs to cool long enough to get to the runway. Put= some=20 tufts on wires right behind the prop and long enough to get into the duct= ing. I=20 bet almost nothing flows into the ducting. Mount a pancake fan behind the= =20 radiator to cool on the ground. Some of the spiral flow from the prop will= =20 defeat the straight sides of the ducting. Ram air at flying speed is=20 completely different. Most added temperature shows up in the oil with hig= h power=20 settings. The racer cooling at low speed is just not adequate. But once= you=20 hit the first straight and go over 100 MPH (top speed 146) the cooling is great. Make one change at a time. Make it= a =20 big change. Record the instruments on video. Just like running the dyno.= =20 Run a bit rich on the ground. Say 1600 degrees or less EGT. This will hel= p a=20 bit.=20 Lynn E. Hanover =20 =20 In a message dated 12/28/2017 7:55:29 P.M. Eastern Standard Time, =20 flyrotary@lancaironline.net writes: Steve I suspect it=E2=80=99s #2. Steve B=E2=80=99s email has a wealth of inform= ation and points=20 to airflow. To prove it layup a quick but reasonable shaped duct and test= =20 it with the cowl off. I would start with a 28 sq or large inlet. 30% of= the=20 core face would be a good place to start testing. =20 I=E2=80=99ve only seen Tracy takeoff in the RV8 once. But he was not using= =20 anywhere near full throttle. He did a lot of work on the inlets but I=E2= =80=99m not sure=20 he can use all 300HP in the summer. =20 Bobby Sent from my iPad > On Dec 28, 2017, at 5:13 PM, Stephen Izett stephen.izett@gmail.com =20 wrote: >=20 > Hi Guys > =20 > Thanks for the replies >=20 > Our water inlet is small (Standard Glasair) - modelled of Tracy=E2=80= =99s RV8=20 20b=20 > I understood he had a round right cheek inlet of 5.25=E2=80=9D giving= him 22=20 in^2 to his water rad for 300hp in Florida temps.=20 > For the two rotor -> 2/3rd of 22 is <15. We have >16 for <200hp >=20 > My concern is the delta T=E2=80=99s. > Yesterday at 1800rpm I was seeing 12F across oil and 6F across the=20 water. Previously I=E2=80=99d seen this as high as 18F and 9F not sure why= so low =20 yesterday. > What do others see on the ground at idle? > Does anyone have good pressure data on the ground. Idle and power=20 settings? > =20 > Are these low due to: > 1. Water flow due to cooling system design or air trapped. > 2. Air flow due to small inlet, compounded by a prop that doesn=E2=80= =99t have=20 much blade near the spinner.=20 >=20 > I=E2=80=99ll look at some further baffling of the Rad to exit but cant= see this=20 helping at idle air speeds unless I duct the exit low pressure direct to= =20 the back of the core. >=20 > I=E2=80=99ll send further photos > Thanks > Steve >=20 > Steve<3.JPG> > -- Homepage: http://www.flyrotary.com/ Archive and UnSub: =20 http://mail.lancaironline.net:81/lists/flyrotary/List.html --part1_c718c.5244be7a.4776fd6a_boundary Content-Type: text/html; charset="UTF-8" Content-Transfer-Encoding: quoted-printable Content-Language: en
Are these cooling tests being done at speed, say 60 to 70 MPH? Or,=20 stationary?  It only needs to cool long enough to get to the runway.= Put=20 some tufts on wires right behind the prop and long enough to get into the= =20 ducting. I bet almost nothing flows into the ducting. Mount a pancake fan= behind=20 the radiator to cool on the ground. Some of the spiral flow from the prop= will=20 defeat the straight sides of the ducting. Ram air at flying speed is compl= etely=20 different. Most added temperature shows up in the oil with high power sett= ings.=20 The racer cooling at low speed is just not adequate. But once you hit the= first=20 straight and go over 100 MPH
(top speed 146) the cooling is great. Make one change at a time. Make= it a=20 big change. Record the instruments on video. Just like running the dyno.= Run a=20 bit rich on the ground. Say 1600 degrees or less EGT. This will help a bit= .=20
Lynn E. Hanover
 
In a message dated 12/28/2017 7:55:29 P.M. Eastern Standard Time,=20 flyrotary@lancaironline.net writes:
Steve

I suspect it=E2=80=99s #2. Steve B=E2=80=99s= email has a wealth of=20 information and points to airflow. To prove it layup a quick but reasona= ble=20 shaped duct and test it with the cowl off. I would start with a 28 sq or= large=20 inlet. 30% of the core face would be a good place to start testing.=20

I=E2=80=99ve only seen Tracy takeoff in the RV8 once. But he was= not using=20 anywhere near full throttle. He did a lot of work on the inlets but I=E2= =80=99m not=20 sure he can use all 300HP in the summer. =20

Bobby



Sent from my iPad

> On Dec 28, 20= 17, at=20 5:13 PM, Stephen Izett stephen.izett@gmail.com=20 <flyrotary@lancaironline.net> wrote:
>
> Hi Guys
&= gt;=20
> Thanks for the replies
>
> Our water inlet is smal= l=20 (Standard Glasair) - modelled of Tracy=E2=80=99s RV8 20b
> I unde= rstood he had=20 a round right cheek inlet of 5.25=E2=80=9D giving him 22 in^2 to his wat= er rad for=20 300hp in Florida temps.
> For the two rotor -> 2/3rd of 22 is= =20 <15. We have >16 for <200hp
>
> My concern is the= delta=20 T=E2=80=99s.
> Yesterday at 1800rpm I was seeing 12F across oil an= d 6F across=20 the water. Previously I=E2=80=99d seen this as high as 18F and 9F not su= re why so low=20 yesterday.
> What do others see on the ground at idle?
> Doe= s=20 anyone have good pressure data on the ground. Idle and power settings?>=20
> Are these low due to:
> 1. Water flow due to cooling syst= em=20 design or air trapped.
> 2. Air flow due to small inlet, compounde= d by a=20 prop that doesn=E2=80=99t have much blade near the spinner.
> > I=E2=80=99ll=20 look at some further baffling of the Rad to exit but cant see this helpi= ng at=20 idle air speeds unless I duct the exit low pressure direct to the back= of the=20 core.
>
> I=E2=80=99ll send further photos
> Thanks>=20 Steve
>
> Steve<3.JPG>
> <Cowl=20 exit.jpg>

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