X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=PNVxBsiC c=1 sm=1 tr=0 a=fRobNB4176/1vJkX6jXp/g==:117 a=55z/sxGcUIPVrBMYBb4HRw==:17 a=jpOVt7BSZ2e4Z31A5e1TngXxSK0=:19 a=x7bEGLp0ZPQA:10 a=_Z_nqdSeG58A:10 a=FmdZ9Uzk2mMA:10 a=r77TgQKjGQsHNAKrUKIA:9 a=pGLkceISAAAA:8 a=7g1VtSJxAAAA:8 a=Ia-xEzejAAAA:8 a=-uMM6Ssdst3bDXM6JCwA:9 a=uHFXurHCk1BDaxvH:21 a=08dQJxiPBzF10RIH:21 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=4PR2P7QzAAAA:8 a=HgsoyHWEwq8tMV__urMA:9 a=tW9xVAjR_VWqdYep:21 a=8i7tZ_K8jFx1Gl2W:21 a=XyfbelSFl23jnPU9:21 a=_W_S_7VecoQA:10 a=grOzbf7U_OpcSX4AJOnl:22 a=Urk15JJjZg1Xo0ryW_k8:22 a=4dqwQCo7Po2mVW515mGf:22 From: "Neil Unger 12348ung@gmail.com" Received: from mail-pf1-f170.google.com ([209.85.210.170] verified) by logan.com (CommuniGate Pro SMTP 6.2.13) with ESMTPS id 12848346 for flyrotary@lancaironline.net; Thu, 15 Aug 2019 02:59:20 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.210.170; envelope-from=12348ung@gmail.com Received: by mail-pf1-f170.google.com with SMTP id d85so929443pfd.2 for ; Wed, 14 Aug 2019 23:59:22 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=subject:to:references:from:message-id:date:user-agent:mime-version :in-reply-to:content-language; bh=N4LF5WsQiW6ptEBM5UqFDvbuG6kQ1frBTy2uJbrL3yE=; b=Ua9DkMuO5lPJUWixhEoj5QWNNRph2HcG9UdvEofKpwVLRU/vz/w8SXKCpRGmTUMs1c ChWJ+qsDgpyHzDRpvWEiWQnFJqZZTdIFtGOXr00hLB4aQtdzOUNJP+aIaVXB/tuW9ZRt 0Q5Xmqo42UgtGPneeDmTH3Rb4Ya7W/wMTS616jWw5VuP+xePIQ/06OoEH14/19LyqYcy FEhzuNKvbI+LfqfErPWOITqHiDjeekBl4c8Gb8Wg2Skq+bGX01WXNeAb1TGQpoj6i6q8 C+OVbuiZE2U741VivVMHTioGWs/C4XUXbpV0EPHbZm3mdBdNAlwZAODrvLp//TH0Zd49 5Ngg== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:subject:to:references:from:message-id:date :user-agent:mime-version:in-reply-to:content-language; bh=N4LF5WsQiW6ptEBM5UqFDvbuG6kQ1frBTy2uJbrL3yE=; b=qgCz5BtbWwMM2slgoXUxEcYmprWlc9Dasly7iJ/vHkXEpPDPKPOR8ouv7btUcMoVpV k4rOVYJM7xabUPObKqt5aS9g02YNE4A67XInQVF08WjrI5R2Q5pDYaiauZKdSmnKttC+ wgxcRCt3qwMX/hmAEt9Lb4uxwZzL2saAfDrZzx1bLZRqYf7IJdWcENpmaiclfqHpXuWw PmbUkpFRX9gzbCeF1XfoGlLznDQrARpy5l6iHNC4oCRbtgkbj4KOGZ8itJfzC5+ragn2 gpRD1bQGxaRcGKdg3iWTdEBrgwQbh0/5l29SYhNGDEDqjfUBj1w+dH5Vg3Efp72JrrIC 2KQw== X-Gm-Message-State: APjAAAVBEHVj8XdunmC+b/rB9LHUzAzgfvo1AyHGkjNc5RNuCxYwd2ZM YKM7KNZssxitSRC0lF2vMA9MXKaS X-Google-Smtp-Source: APXvYqyrsss8psU4cSHFE4qaulsO2GhThNy9oQywEtkXxxaWUcvru/XTAbIE89/ul/9jiin4feuwAQ== X-Received: by 2002:a63:fc52:: with SMTP id r18mr2425712pgk.378.1565852343679; Wed, 14 Aug 2019 23:59:03 -0700 (PDT) Return-Path: <12348ung@gmail.com> Received: from [192.168.0.106] ([103.198.24.78]) by smtp.gmail.com with ESMTPSA id p4sm237128pjr.14.2019.08.14.23.59.02 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Wed, 14 Aug 2019 23:59:03 -0700 (PDT) Subject: Re: [FlyRotary] Inlet duct sizing To: Rotary motors in aircraft References: Message-ID: <31c02034-fb3e-bd43-97e2-f07d817488f5@gmail.com> Date: Thu, 15 Aug 2019 16:58:58 +1000 User-Agent: Mozilla/5.0 (Windows NT 10.0; WOW64; rv:60.0) Gecko/20100101 Thunderbird/60.8.0 MIME-Version: 1.0 In-Reply-To: Content-Type: multipart/alternative; boundary="------------3FC98BE2768370A531676D2F" Content-Language: en-US This is a multi-part message in MIME format. --------------3FC98BE2768370A531676D2F Content-Type: text/plain; charset=utf-8; format=flowed Content-Transfer-Encoding: 8bit Mat,  measurements are not exact as I have a cowl in the way, but basically I have 90 sq inches  total air  inlet which is divided up 1/3  2/3 between oil and water.  Cubic inches for oil is 8 x 18 x 2.25 equals 324 cubic inches for oil.  Water is 13 x 20 x 2.25 giving 585 cubs. I find this is just good enough in our 105 degrees F  summer heat.  Now in winter it takes 10 minutes to heat the water to 80 degrees on the thermostat.  Oil is flat to get to 70 degrees, but it is only about 60 degrees OAT .  I feel a lot of you blokes seem to get away with very small radiators, but My Rad is the smallest I would be comfortable with in our summers. Will be interesting to see how you go. Regards Neil. On 8/15/2019 1:42 PM, Matt Boiteau mattboiteau@gmail.com wrote: > I'm having a hard time in this Florida heat, trying to do my first > flight. With a highspeed taxi run, (up to 55kts or so), will net my > oil and coolant above my warning limits. 240 oil pan, 230 coolant out. > > The coolant inlet (44sq") is huge with the idea that down the road I'd > go turbo. The rad is from a dodge truck 19 x 24 x 1 = 454sq", with a > wedge shape diffuser. Right now it just exits the back of the cowl, no > cowl flaps or sub cowl installed yet. > > The oil inlet is a lot smaller (~12.5sq"), going to a 2.5" scat hose, > then to a trumpet shape which leads into a wedge. The oil rad is 9 x > 11 x 2 = 198sq" from cx racing. For the outlet, I have a big box to > collect the hot/expanded air, then neck it back down to 2.5" exit. > Tomorrow I'll try another taxi test, with the outlet box > completely removed and dumping into the cowl. > > To find out if my prop is doing anything with airflow into the inlets, > used a tube of water and found around 2200 static rpm, it raised the > water about 4inches in the oil duct. I think that equals around > ~55kts. I thought the prop would of cooled down the rads a lot more, > but I guess I have bad duct designs. Maybe move them closer to the > blade? Looking at the picture, the oil is on the left with all the > green tape. I tried to make the opening bigger with foam, didn't see a > real difference. Being on the bottom of the cowl and to the left, it > doesn't get the rotating air from the blades as much. > > I know high speed taxi tests in this Florida heat, is probably the > worst case scenario. Depending how the morning goes, we might just fly > the plane and get some speed into her nose. See at what speed the > temperatures stabilize and start to cool down. > > - Matt Boiteau > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html --------------3FC98BE2768370A531676D2F Content-Type: text/html; charset=utf-8 Content-Transfer-Encoding: 8bit

Mat,  measurements are not exact as I have a cowl in the way, but basically I have 90 sq inches  total air  inlet which is divided up 1/3  2/3 between oil and water.  Cubic inches for oil is 8 x 18 x 2.25 equals 324 cubic inches for oil.  Water is 13 x 20 x 2.25 giving 585 cubs.

I find this is just good enough in our 105 degrees F  summer heat.  Now in winter it takes 10 minutes to heat the water to 80 degrees on the thermostat.  Oil is flat to get to 70 degrees, but it is only about 60 degrees OAT .  I feel a lot of you blokes seem to get away with very small radiators, but My Rad is the smallest I would be comfortable with in our summers.

Will be interesting to see how you go.

Regards Neil.

On 8/15/2019 1:42 PM, Matt Boiteau mattboiteau@gmail.com wrote:
I'm having a hard time in this Florida heat, trying to do my first flight. With a highspeed taxi run, (up to 55kts or so), will net my oil and coolant above my warning limits. 240 oil pan, 230 coolant out.

The coolant inlet (44sq") is huge with the idea that down the road I'd go turbo. The rad is from a dodge truck 19 x 24 x 1 = 454sq", with a wedge shape diffuser. Right now it just exits the back of the cowl, no cowl flaps or sub cowl installed yet.

The oil inlet is a lot smaller (~12.5sq"), going to a 2.5" scat hose, then to a trumpet shape which leads into a wedge. The oil rad is 9 x 11 x 2 = 198sq" from cx racing. For the outlet, I have a big box to collect the hot/expanded air, then neck it back down to 2.5" exit. Tomorrow I'll try another taxi test, with the outlet box completely removed and dumping into the cowl.

To find out if my prop is doing anything with airflow into the inlets, used a tube of water and found around 2200 static rpm, it raised the water about 4inches in the oil duct. I think that equals around ~55kts. I thought the prop would of cooled down the rads a lot more, but I guess I have bad duct designs. Maybe move them closer to the blade? Looking at the picture, the oil is on the left with all the green tape. I tried to make the opening bigger with foam, didn't see a real difference. Being on the bottom of the cowl and to the left, it doesn't get the rotating air from the blades as much.

I know high speed taxi tests in this Florida heat, is probably the worst case scenario. Depending how the morning goes, we might just fly the plane and get some speed into her nose. See at what speed the temperatures stabilize and start to cool down.

- Matt Boiteau

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