X-Virus-Scanned: clean according to Sophos on Logan.com From: "Bobby J. Hughes" Received: from [66.219.56.245] (HELO mail.qnsi.net) by logan.com (CommuniGate Pro SMTP 6.1.2) with ESMTP id 7695666 for flyrotary@lancaironline.net; Sat, 16 May 2015 10:31:50 -0400 Received-SPF: pass receiver=logan.com; client-ip=66.219.56.245; envelope-from=bhughes@qnsi.net X-MimeOLE: Produced By Microsoft Exchange V6.5 Content-class: urn:content-classes:message Return-Receipt-To: "Bobby J. Hughes" MIME-Version: 1.0 Content-Type: multipart/mixed; boundary="----_=_NextPart_001_01D08FE4.F7334DB9" Subject: RE: [FlyRotary] Re: Return to Flight - 2 Disposition-Notification-To: "Bobby J. Hughes" Date: Sat, 16 May 2015 09:31:13 -0500 Message-ID: <74120FDE88CAFE4DBDA8814BCE20A3F3907AAB@qnsi-mail.qnsi.net> In-Reply-To: X-MS-Has-Attach: yes X-MS-TNEF-Correlator: Thread-Topic: [FlyRotary] Re: Return to Flight - 2 Thread-Index: AdCPgeBqaouE37ajRtyDVJfL0aMXXgAXH9FA References: To: "Rotary motors in aircraft" This is a multi-part message in MIME format. ------_=_NextPart_001_01D08FE4.F7334DB9 Content-Type: multipart/related; boundary="----_=_NextPart_002_01D08FE4.F7334DB9"; type="multipart/alternative" ------_=_NextPart_002_01D08FE4.F7334DB9 Content-Type: multipart/alternative; boundary="----_=_NextPart_003_01D08FE4.F7334DB9" ------_=_NextPart_003_01D08FE4.F7334DB9 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Jeff, =20 I 'll share how poor the air distribution actually is for my two radiators. The attachment shows three tests with changes to guiding vane placements. The bottom measurements are what I'm flying now. I am turning the air 90 degrees right before the wedge entrance so that's why the airspeed is so slow in that area. I don't have enough room for a more graceful turn and didn't find a better solution. I'm cooling 38" MP on a 95F day to pattern altitude with water temps around 215. Once power is reduced the water temp drops quickly. The core exit airspeed map shows what Charlie is point out.=20 =20 If you can make a big change first try removed the exit wedge. I've been told we need 12" of clear space behind our heat exchangers . Dennis H. and I did some testing several years ago and I remember we observed a negative impact to airflow by placing a sheet of aluminum or cardboard at the core exit. We checked different distances but don't remember if 12" was the magic number.=20 =20 =20 =20 Good luck =20 Bobby =20 =20 =20 From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net]=20 Sent: Friday, May 15, 2015 10:43 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Return to Flight - 2 =20 Hi Jeff, First, a caution: I'm a long way from flying, so this is untested in flight.=20 But I did a similar thing to what Bobby said, and used a leaf blower to pressurize my rad plenum. I used a thread on a stick to check outflow from the rad core. Looking at the drawing of your wedge plenum, I'd bet that almost all the air is coming out the last 5 or 8 inches of the core. Before I made mine, I asked Tracy about his RV-8 plenum. He said to pinch the back down tight; that he had to stuff open cell foam in the back of his to even the flow, so I did (I thought). He happened to be here as I was getting ready to glass the mold, and commented that it was probably too thick at the rear. (It was *much* tighter than your drawing shows.) Sure enough, when I checked flow, all the air came through the rear of the core. To get even flow from front to back, I re-shaped the inside of the wedge until the last couple of inches almost touch the core. Also, in order to spread flow across the core (side to side, perpendicular to the inlet flow), I had to install a turning vane in the inlet duct. For reference, I'm building an RV-7 with a Sam James cowl made for a Lyc; not the rotary cowl with a chin inlet for the rad. So my ~4.5" round inlet transitions to more or less rectangular cross section with slightly increased area where it arrives at the front edge of the core. Then it's a concave wedge, pinching down to almost a knife edge at the back end of the core. No idea if it will actually cool, but I do know that the airflow coming out of the core is pretty evenly balanced when using the leaf blower to push air through it. Pics below. The trailing edge is a lot thinner than it looks, because there's 'filler' on the inside to thin the wedge. FWIW... Charlie http://s1155.photobucket.com/user/rv7charlie/media/1d6b1e19.jpg.html http://s1155.photobucket.com/user/rv7charlie/media/slobovia12a_zps319477 7e.jpg.html http://s1155.photobucket.com/user/rv7charlie/media/pdrop2012_zpscbc0ae13 .jpg.html http://s1155.photobucket.com/user/rv7charlie/media/4seatback_zps033399e2 .jpg.html http://s1155.photobucket.com/user/rv7charlie/media/Slobovia14_zps413ea84 e.jpg.html On 5/15/2015 2:17 PM, Jeff Whaley wrote: Actually I don't have any really good pictures because I took it apart ... but attached is a side-view after removal of the inlet diffuser on top and also a sketch of approximate scale and shape of what I tried to make, (I don't have a damper plate or cowl flap yet). The top shape isn't quite right; needs to be pinched more at the rear, also am considering a turning vane to direct more air through the front half. Trying to make air bend 90 degrees twice isn't easy but I chose this orientation because of the desire to add a damper at the output for winter operations. I could drop the rear of radiator and bring air in through the bottom, spilling out over the engine but would lose the ability to have a damper - I don't like the idea of inlet dampers. On top of it all, my climb speed is usually only 90 mph; I don't have the ability to get extra pressure from increased airspeed. P.S. the radiator is the Griffin 2-58185-X, same as several other installs on this list. The top plenum was out in the SUV; hopefully more attachments in next post ... Jeff =20 From: David Leonard =20 Subject: Re: [FlyRotary] Return to Flight - 2 Date: Fri, 15 May 2015 09:48:38 -0700 To: Rotary motors in aircraft =20 =20 =20 Sorry to hear that Jeff. My apologies if you have already posted pictures of the your installation and the diffuser, but could you post some now? =20 Dave Leonard =20 On Fri, May 15, 2015 at 8:19 AM, Jeff Whaley < flyrotary@lancaironline.net> wrote: From: Jeff Whaley=20 Sent: Friday, May 15, 2015 11:19 AM To: 'Bobby J. Hughes' Subject: Return to Flight - 2 =20 Well, the second flight occurred last night with same results as before; one short low-level circuit due to insufficient cooling ... looks like Al Wick made the correct prediction. There are 3 things I can try with the current configuration: 1) Increase inlet area 2) Increase outlet area (adjustable cowl flap) 3) Re-profile the pinched diffuser. I will do all 3 and see what happens. If all of the above show remarkable improvement then repositioning the radiator is the only alternative. Jeff This message, and the documents attached hereto, is intended only for the addressee and may contain privileged or confidential information. Any unauthorized disclosure is strictly prohibited. If you have received this message in error, please notify us immediately so that we may correct our internal records. Please then delete the original message. Thank you.=20 =09 =09 =09 -- Homepage: http://www.flyrotary.com/ Archive and UnSub: =20 http://mail.lancaironline.net:81/lists/flyrotary/List.html =20 ------_=_NextPart_003_01D08FE4.F7334DB9 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Jeff,

 

I ‘ll share how poor the air distribution actually is for my = two radiators. The attachment shows three tests with changes to guiding = vane placements. The bottom measurements are what I’m flying now. = I am turning the air 90 degrees right before the wedge entrance so = that’s why  the airspeed is so slow in that area. I = don’t have enough room for a more graceful turn and didn’t = find a better solution.   I’m  cooling 38” MP = on a 95F day to pattern altitude with water temps around 215. Once power = is reduced the water temp drops quickly. The core exit airspeed map = shows what Charlie is point out.

 

If you can make a big change first try removed the exit wedge. = I’ve been told we need 12” of clear space behind our heat = exchangers . Dennis H. and I did some testing several years ago and I = remember we observed a  negative impact to airflow by placing a = sheet of aluminum or cardboard at the core exit. We checked different = distances but don’t remember if 12” was the magic number. =

 

 

 

Good luck

 

Bobby

 

 

 

From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] =
Sent: Friday, May 15, 2015 10:43 PM
To: Rotary = motors in aircraft
Subject: [FlyRotary] Re: Return to Flight - = 2

 

Hi = Jeff,

First, a caution: I'm a long way from flying, so this is = untested in flight.

But I did a similar thing to what Bobby = said, and used a leaf blower to pressurize my rad plenum. I used a = thread on a stick to check outflow from the rad core. Looking at the = drawing of your wedge plenum, I'd bet that almost all the air is coming = out the last 5 or 8 inches of the core. Before I made mine, I asked = Tracy about his RV-8 plenum. He said to pinch the back down tight; that = he had to stuff open cell foam in the back of his to even the flow, so I = did (I thought). He happened to be here as I was getting ready to glass = the mold, and commented that it was probably too thick at the rear. (It = was *much* tighter than your drawing shows.) Sure enough, when I checked = flow, all the air came through the rear of the core. To get even flow = from front to back, I re-shaped the inside of the wedge until the last = couple of inches almost touch the core.

Also, in order to spread = flow across the core (side to side, perpendicular to the inlet flow), I = had to install a turning vane in the inlet duct. For reference, I'm = building an RV-7 with a Sam James cowl made for a Lyc; not the rotary = cowl with a chin inlet for the rad. So my ~4.5" round inlet = transitions to more or less rectangular cross section with slightly = increased area where it arrives at the front edge of the core. Then it's = a concave wedge, pinching down to almost a knife edge at the back end of = the core.

No idea if it will actually cool, but I do know that = the airflow coming out of the core is pretty evenly balanced when using = the leaf blower to push air through it.

Pics below. The trailing = edge is a lot thinner than it looks, because there's 'filler' on the = inside to thin the wedge.

FWIW...

Charlie

http://s1155.photobucket.com/user/rv7charlie/media/1d6b1e19.jpg.html=
http://s1155.photobucket.com/user/rv7charlie/media/sl= obovia12a_zps3194777e.jpg.html
http://s1155.photobucket.com/user/rv7charlie/media/pdro= p2012_zpscbc0ae13.jpg.html
http://s1155.photobucket.com/user/rv7charlie/media/4sea= tback_zps033399e2.jpg.html
http://s1155.photobucket.com/user/rv7charlie/media/Slo= bovia14_zps413ea84e.jpg.html


On 5/15/2015 2:17 PM, Jeff = Whaley wrote:

Actually I don’t have any really good pictures because I took = it apart … but attached is a side-view after removal of the inlet = diffuser on top and also a sketch of approximate scale and shape of what = I tried to make, (I don’t have a damper plate or cowl flap = yet).  The top shape isn’t quite right; needs to be pinched = more at the rear, also am considering a turning vane to direct more air = through the front half.  Trying to make air bend 90 degrees twice = isn’t easy but I chose this orientation because of the desire to = add a damper at the output for winter operations.  I could drop the = rear of radiator and bring air in through the bottom, spilling out over = the engine but would lose the ability to have a damper – I = don’t like the idea of inlet dampers.  On top of it all, my = climb speed is usually only 90 mph; I don’t have the ability to = get extra pressure from increased airspeed.   P.S. the = radiator is the Griffin 2-58185-X, same as several other installs on = this list.

The top plenum was out in the SUV; hopefully more attachments in next = post …

Jeff

 

From:

David Leonard <flyrotary@lancaironline.n= et>

Subject:

Re: = [FlyRotary] Return to Flight - 2

Date:

Fri, 15 May 2015 09:48:38 = -0700

To:

Rotary = motors in aircraft <flyrotary@lancaironline.n= et>

3D"Message

3D"Undecoded

Sorry to hear that Jeff.  My apologies if you = have already posted pictures of the your installation and the diffuser, = but could you post some now?

 

Dave = Leonard

 

On Fri, May 15, 2015 at 8:19 AM, Jeff Whaley <flyrotary@lancaironline.net> = wrote:

From:= = Jeff Whaley
Sent: Friday, May 15, 2015 11:19 AM
To: = 'Bobby J. Hughes'
Subject: Return to Flight - = 2

 

Well, the second flight occurred last night with same results as = before; one short low-level circuit due to insufficient cooling … = looks like Al Wick made the correct prediction.

There are 3 things I can try with the current configuration: 1) = Increase inlet area 2) Increase outlet area (adjustable cowl flap) 3) = Re-profile the pinched diffuser.  I will do all 3 and see what = happens.

If all of the above show remarkable improvement then repositioning = the radiator is the only alternative.

Jeff

This message, and the = documents attached hereto, is intended only for the addressee and may = contain privileged or confidential information. Any unauthorized = disclosure is strictly prohibited. If you have received this message in = error, please notify us immediately so that we may correct our internal = records. Please then delete the original message. Thank you. = 


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

 

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