X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.2 cv=L5hfeKb8 c=1 sm=1 tr=0 a=Fn4HpnRQkMeKTtx/PkYqpg==:117 a=tjnKUyPNcBkiZvAAz0wTOw==:17 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=v2DPQv5-lfwA:10 a=pGLkceISAAAA:8 a=Ia-xEzejAAAA:8 a=_6GpL_ENAAAA:8 a=7g1VtSJxAAAA:8 a=1zHGzOJbIHjEJQMEZGcA:9 a=QEXdDO2ut3YA:10 a=FMnVVNC4FTgA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=T_WObCaBjb5lLww25dKY:22 a=Urk15JJjZg1Xo0ryW_k8:22 a=grOzbf7U_OpcSX4AJOnl:22 From: "Stephen Izett stephen.izett@gmail.com" Received: from mail-pg0-f53.google.com ([74.125.83.53] verified) by logan.com (CommuniGate Pro SMTP 6.2.2) with ESMTPS id 10871050 for flyrotary@lancaironline.net; Fri, 23 Mar 2018 20:16:22 -0400 Received-SPF: pass receiver=logan.com; client-ip=74.125.83.53; envelope-from=stephen.izett@gmail.com Received: by mail-pg0-f53.google.com with SMTP id n11so5172978pgp.4 for ; Fri, 23 Mar 2018 17:16:23 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=from:content-transfer-encoding:mime-version:subject:date:references :to:in-reply-to:message-id; bh=vOcaXa6fqojp+XO+gV69+5Qz2xvCkGwQLDihA4Oz2iU=; b=sR5HLakeAql9C9DU4D3OHhX/iFSIDnYjutLB0pUbW+/EezqOEflHyp0rrpUtmJ0CYV 7+qOvfzku/xa6h7qQEMN87/NWtUaqw48zkIlQ7Scy0vnMziRs/yh6+dW8BZj1zrHOEBz JZap7sVhlH7YfgM+xNVFg4tVbRyEJIjMcJ1OpI3jFczlKzqpEW/0F+RQIWqavqkX/c+W rNEF72qnru3Sj9ZN483FdzpG2C4Ij/lqGhxAnqUwQ3bKuA4BRlBxbJq1XIHMId97Mfr4 JMryQ0P5PZQLTEbRFfBOij9rhIrTXM/QRoda5jTp+wM5c4iT67Cc+gpQaaubZppMbXe3 MThw== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:from:content-transfer-encoding:mime-version :subject:date:references:to:in-reply-to:message-id; bh=vOcaXa6fqojp+XO+gV69+5Qz2xvCkGwQLDihA4Oz2iU=; b=JDzGo4fWfHbm5D7xqC9isTVEMQ2A9T95NBdqowK/ZATSSdQoAl1o+OO0jTYRRp7vk6 EPHo2RVNp7fUBrHCUAK6Zo/xjtFNIurB9DnD3zYB+TGfyyD4Uw58dz77GJFRpTGBIjRC MyRspfHNzm6kCDrSGqjJbKNuyGg2TOSnL8jDumvkpgmNp3qyXHJqtQYMGRQXVNJYhSyS bMf+/rV4gkOuTN9n+FxPhNDhUuRFmjZ17Mq5aLDcnpEXYtb1CyRbTTNb6rZreeco6JrD LP334VTbJtwoSGFFzn4Ksv28q4PeVATQyYPo7M+S0NVznTSGw/JrsNzYicENJKCEx8ku XAuA== X-Gm-Message-State: AElRT7HINEJUC8AgjFtOTpIWCu8fpBYEzWinEfBheqefLY8j+zDH2erD 35QEVc0VyBQeNSRcE4kdsb1J22hO X-Google-Smtp-Source: AG47ELvfopodCQOoIYMqmJzNkaUlsQMaIyKaBtR2yn8qhWFrKemuA3bgIAts2AtnrsPyaHgHI/lx3w== X-Received: by 10.101.92.76 with SMTP id v12mr22202046pgr.50.1521850564585; Fri, 23 Mar 2018 17:16:04 -0700 (PDT) Return-Path: Received: from steves-mbp.lan ([118.208.177.246]) by smtp.gmail.com with ESMTPSA id f82sm21978098pfd.175.2018.03.23.17.16.02 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Fri, 23 Mar 2018 17:16:04 -0700 (PDT) Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (Mac OS X Mail 10.3 \(3273\)) Subject: Re: [FlyRotary] Re: Glasair Testing Continued Date: Sat, 24 Mar 2018 08:16:01 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <9A46CBC6-968F-47D0-9D9F-5C44BAFF6E61@gmail.com> X-Mailer: Apple Mail (2.3273) > On 23 Mar 2018, at 10:24 pm, Tracy Crook rwstracy@gmail.com = wrote: >=20 > Haven=E2=80=99t had occasion to test the RV-8 this way but on an 85 F = day my RV-4 will eventually get up to about 224F (oil and gas) while = taxiing and stabilize there. This does not harm the engine at all. But = if I were to start a takeoff roll at that temp the coolant will boil = during a normal climb out. If I nurse it carefully (minimum climb rate = & best cooling airspeed of 125 mph) it will start cooling down before = boiling. Never gotten into a situation where this was an operational = problem. > =20 > Tracy > =20 > =20 > =20 > Sent from Mail for Windows 10 > =20 > From: Stephen Izett stephen.izett@gmail.com > Sent: Friday, March 23, 2018 10:05 AM > To: Rotary motors in aircraft > Subject: [FlyRotary] Re: Glasair Testing Continued > =20 > Hi Charlie > I do use Maximite, actually these days Geoff=E2=80=99s lattest = Micromite, just better in every way. > The data is straight out of the Dynon Skyview log. > I will be using a micromite to display and log pressures around the = coolers and cowl etc but haven=E2=80=99t finished the hardware or the = software at this point. > =20 > We will tie it to a tree in the next few weeks so I can check to = mixtures. > I very much doubt it will keep cool at static, she=E2=80=99ll overheat = within I recon 4 minutes at WOT. > Our prop doesn=E2=80=99t;t have much blade close to the spinner where = the water inlet is. The oil inlet is lower and does get better air from = the prop. > =20 > Steve > =20 > > On 23 Mar 2018, at 9:20 pm, Charlie England ceengland7@gmail.com = wrote: > > > > > > > > On Fri, Mar 23, 2018 at 7:35 AM, Stephen Izett = stephen.izett@gmail.com wrote: > > Hi people > > > > I know how much I have appreciated data over the years so for those = interested here is some more. > > Having looked at last weeks test data and the temps looking like = they were close to stabilised after reaching around 212F I thought I = would risk it and see what the temps did get to. > > The temp senders are calibrated accurately up to boiling point = (within <1F at 212F) but I=E2=80=99m not sure how accurate they are up = at 225F. > > The graph below is 43minutes of repeatedly (12 times) taxing and = then running down our ~1000yard strip at between ~20-37knots > > The OAT was 74-77F during this test. > > Renesis 4 port RD1C EC3 EM3 Elect Adj Prop > > Water cooler is 540in3 (custom dual pass) with inlet of 20in2 > > Oil Cooler is 193in3 (mazda rx7 turbo) with inlet of 7.5in2 > > > > I=E2=80=99m wondering what a 30row oil cooler like Tracy uses might = do to both the oil and water temps. > > We will press on and hopefully flight test it as soon as we have it = licensed. > > > > Cheers > > > > Steve Izett > > > > Hi Steve, > > > > Steve Boese has posted some of his pressure differential data on a = Mazda cooler. He was seeing a really large oil pressure drop across the = cooler, indicating highly restricted flow through it. Less flow=3Dless = cooling. Have you measured oil pressures on the inlet and outlet? > > > > As Tracy has mentioned in the past, short bursts of power won't = really tell you much relative to sustained high power. Too many = variables: inconsistent heat input, and inconsistent air flow for = cooling (varying speeds). Since you have a controllable prop, have you = tried tying the plane down & doing a sustained run at, say, 75% power? = Surely the plane would get off the ground using 75% power, so if you can = cool with static (only the prop) airflow into your heat exchangers, = flying speeds will only help with cooling mass flow through the coolers. > > > > Are you the one using a Maximite to gather your data? If so, would = you be willing to share your code? I can handle most things electronic, = but I'm not any kind of coder at all. :-) > > > > Charlie > > > > Virus-free. www.avast.com > =20 > =20 > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html