X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.2 cv=eqSd9chX c=1 sm=1 tr=0 a=OEVJYw/obVdrmk2EYfkxnA==:117 a=KJU6LNLacHgTudGz15/Qvg==:17 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=Kd1tUaAdevIA:10 a=pGLkceISAAAA:8 a=Ia-xEzejAAAA:8 a=_6GpL_ENAAAA:8 a=7g1VtSJxAAAA:8 a=n7QPQOdQED3hN9VDjB0A: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-pf0-f182.google.com ([209.85.192.182] verified) by logan.com (CommuniGate Pro SMTP 6.2.2) with ESMTPS id 11067762 for flyrotary@lancaironline.net; Sun, 29 Apr 2018 02:55:37 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.192.182; envelope-from=stephen.izett@gmail.com Received: by mail-pf0-f182.google.com with SMTP id f15so4455548pfn.0 for ; Sat, 28 Apr 2018 23:55:39 -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=Odv1Ngw8Xzn/wFbglyiY/GZUw9iO/SKk9R8mnTmu/b4=; b=QaRDQnKaqjaNCU9rHG3XkL1+0P7uxb/kuaDg2T/IhzjNeAeT5yRxQURA+vJhGpfMiy PNg/PEiYmBh+S9G1iRwuR6XeRvtxdUOzqS8jQdrbqJzdeLe4BD/reTAMLE9qRQvQGbpF LTGvR3HiPFuZiHnEvvWyQFVGad4uF2wix+jJq6AmIH84XFSBUp46k0LMliTvZK77JtGl oQCmMHOugmklZU+byD+ZdUYVLoizwvvuhyQzlOYHQSJpcx1nQl7kWjiqqLtaatNdWR+U FeaeizFGYS5oSFModrR6ztb2AYqA/EiWEWFi1HQ6CW0E0j155h/GJ959qJ8ZQzgzdyyY xdCA== 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=Odv1Ngw8Xzn/wFbglyiY/GZUw9iO/SKk9R8mnTmu/b4=; b=k6rm4N/H2imFcUka6HGNf/jTYfVzE4du/FuOpPFljboOCgBi7Abs5PYmm4d5mP+VtT oaOxiWzTej1g+nqpchFgdeJgj00eicLfVEYt1g1sGh2O8u7p73HgWdftue4pgL5Zb4Q+ qF5ljLXz8dtsftbnGNZj9QR2k/sSRlrQiwvi14cjwHOAVZzBJTpwE24Y5gzAS/stApHC M2YU369I/F6WU6oqFphWzAzELXZ19+tEBLIWMhjribiZc3W0ITr7CPyjsWrSZ3l1kwJw kLYizURiVQFLuKa7yOxXQEaF/X4ncuTRhAgY8TTO1JmExtiBU+zO0b0BDIwmH2lhEkhB UzCQ== X-Gm-Message-State: ALQs6tCA2yDUFwEgQawQWgP/1OVfYMq/bzIzbUrAHSVJpMHzuW3PPyM3 wQmrzjxMTwe0XVKEgQM9LzxynF0b X-Google-Smtp-Source: AB8JxZqP2cbU6HzvAfoMIlwC1msLpBp9cjRZzedrHgk6LF7HeiFBe61FMUElC9I2YLPSXVKmzx2v9Q== X-Received: by 2002:a17:902:548f:: with SMTP id e15-v6mr1622776pli.314.1524984920054; Sat, 28 Apr 2018 23:55:20 -0700 (PDT) Return-Path: Received: from steves-mbp.lan ([118.208.52.183]) by smtp.gmail.com with ESMTPSA id j10sm11964598pfj.1.2018.04.28.23.55.18 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Sat, 28 Apr 2018 23:55:19 -0700 (PDT) Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (Mac OS X Mail 11.3 \(3445.6.18\)) Subject: Re: [FlyRotary] Re: Glasair Testing Continued Date: Sun, 29 Apr 2018 14:55:15 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <9A5E0BEA-4D98-4722-B75A-1260CF7B510C@gmail.com> X-Mailer: Apple Mail (2.3445.6.18) Hi there Todd Sorry, no.=20 Just tidying up some small issues in readiness for licensing. Trim, Wideband O2, decals etc. Our daily temps are heading down so I=E2=80=99m hopeful that when ready = we might get an early morning in the low 50=E2=80=99s F. This hopefully will give us a little more margin with the cooling. Hope to provide more data shortly. Steve Izett > On 29 Apr 2018, at 2:44 pm, Todd Bartrim bartrim@gmail.com = wrote: >=20 > Hi Stephen; > Any news for us? I've been expecting a first flight report any = day now. >=20 > Todd=20 >=20 > On Fri, Mar 23, 2018, 17:16 Stephen Izett stephen.izett@gmail.com, = wrote: >=20 > > On 23 Mar 2018, at 10:24 pm, Tracy Crook rwstracy@gmail.com = wrote: > > > > 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. > > > > Tracy > > > > > > > > Sent from Mail for Windows 10 > > > > 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 > > > > 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. > > > > 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. > > > > Steve > > > > > 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 > > > > > > -- > > Homepage: http://www.flyrotary.com/ > > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html >=20 >=20 > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html