X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.2 cv=as3wMmRV c=1 sm=1 tr=0 a=i2/DfdqvzD4ZxCtt+ESxjA==:117 a=b0WXXb1TpCRXX/ruI2YXbQ==:17 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=ocR9PWop10UA:10 a=Ia-xEzejAAAA:8 a=pGLkceISAAAA:8 a=7g1VtSJxAAAA:8 a=830vuDuJpN8DWD9cswAA:9 a=IdiPeZJGK5EvMXPd:21 a=NDEyDzGKJxOffW3m:21 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=Urk15JJjZg1Xo0ryW_k8:22 a=grOzbf7U_OpcSX4AJOnl:22 From: "Stephen Izett stephen.izett@gmail.com" Received: from mail-pg0-f49.google.com ([74.125.83.49] verified) by logan.com (CommuniGate Pro SMTP 6.2.1) with ESMTPS id 10493092 for flyrotary@lancaironline.net; Fri, 29 Dec 2017 19:04:59 -0500 Received-SPF: pass receiver=logan.com; client-ip=74.125.83.49; envelope-from=stephen.izett@gmail.com Received: by mail-pg0-f49.google.com with SMTP id 81so1916740pgf.6 for ; Fri, 29 Dec 2017 16:05:00 -0800 (PST) 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=zNvIYQYpq/knGI42w8IwS3YL//h1aEdw+W9gWKISGUY=; b=YEvDCJCHgxAGiFeXxUgYdxsw0twiQ8GR74wQLR7Hq1ZX0gXfwifsw35b+6fC9caYIc twJoh7fcb6wLPwVnd9q+QeGw2tEtYkBBPqmz4Iqviu4HafvrqVU5O76dwlnaQwSJKmLq gjtKSc4L43MCvwDXkYBBIC52WGqfEGoMCVv/qh0Q/SJCrWARVkbmEG80mc3jalgnk4hx Cx453bmgzmzQAyj9jHTfrnjJ+cAPaSdwqMk11kF/r4jha1bQhUeviBs96y+GNHgDr14C 7b7tXSMbB5M7AJsTVBbBXutz3adD219BVGE+PAqOFw+pZeFBtVGN7PgOLWGKd/rFqvPf /81Q== 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=zNvIYQYpq/knGI42w8IwS3YL//h1aEdw+W9gWKISGUY=; b=tQMkauObGevBwtRjdMrHTVahKZY24EO1V/EXkzHENQJ9HAFpv+Wc9o5e/CU+HZPKrN 78NLrpVp772EPR0L78dHugrpzoDoX1ukp95S4WfTR95Q/c3MO9d/S2VPg5Dl9ErcdYfD CgKb7LbVriXblGBgfj4T7o8d2kYLwvcCA4PySuu02pcLJmXEpiHPWXhEq7cEzeA7AHli 1Pq2vsCusyCDLDyabhhU6rdOV6GzDDKJqCDkQHBZrkqhVb6stObLvsaHABr9RaBpqPTi UvH1tviKsLpKBkXm157KcdCTIFfrCc6Cl/kMcedKEl6t2WmVTxpC3V9b/uHl4Gd7a64a zeQg== X-Gm-Message-State: AKGB3mLRYNPJKB9CxiCx1U2Vm4cOIveerRz88qqWRFZE8/m1oILDTLQ4 rbkSVZZk5G9xhj3ezZhNTdcem+NF X-Google-Smtp-Source: ACJfBovMDY987AmlnlBJVj5ly3z6BGa/qgxIB3EWHT716AkDwR/uA7CqI6eHIJfD6kCjLwQmSLAt4A== X-Received: by 10.99.140.19 with SMTP id m19mr33018010pgd.47.1514592281484; Fri, 29 Dec 2017 16:04:41 -0800 (PST) Return-Path: Received: from [10.1.1.29] (220-253-221-100.dyn.iinet.net.au. [220.253.221.100]) by smtp.gmail.com with ESMTPSA id u21sm72182615pfl.102.2017.12.29.16.04.39 for (version=TLS1_2 cipher=ECDHE-RSA-AES128-GCM-SHA256 bits=128/128); Fri, 29 Dec 2017 16:04:41 -0800 (PST) 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: Cooling Issues Date: Sat, 30 Dec 2017 08:04:36 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: X-Mailer: Apple Mail (2.3273) Hi there Steve Thanks for the plots. Really interesting. Oil Delta T 33F Water Delta T 15F Cores Delta P 2.6in h2o OAT 70F (21C) hp 42 rpm 4000 Interesting how this test reveals the symbiotic relationship between oil = and water cooling. A drop in oil T of 52F (212-160) caused a 12F drop in the water T A drop in h2o T of 59F (212-153) caused a 10F drop in the oil T So the oil is the bigger player in the system but not massively. (not = very scientific language) I=E2=80=99ll remeasure the duct inlet size accurately. The diffuser entry was laid up into the cowl entry. Then the flange you see in the photo was cut off.=20 The diffuser joins the cowl ~1/2=E2=80=9D inside the cowl lips and then = the cowl lips were micro=E2=80=99d flush with the diffuser. So the diffuser entry sits in a joggle on both upper and lower cowl = lips. These are not sealed with anything, just sit together glass to glass.=20 I=E2=80=99ve wondered how I might get a better seal without using = something like silicon. That cheek also feeds air to cool coils & alternator regulator (you can = see this - right against spinner) which I now plan=20 to feed from the left cheek to increase air to the water rad. What was the load on the test stand and how did you get the Delta P = across the cores? Thanks again. Helpful. Cheers Steve Izett > On 30 Dec 2017, at 4:56 am, Steven W. Boese SBoese@uwyo.edu = wrote: >=20 > Steve, >=20 > The attached plot shows the interaction between coolant and oil = temperatures obtained on my test stand. The oil cooler and the radiator = are fed air from separate ducts and their outlet areas are independently = variable. RPM was 4000 and HP was 42 during the test. Water T is the = temperature of the coolant coming out of the engine and Oil T is oil = temperature returning to the engine from the oil cooler. With those = temperatures stabilized at about 210 deg, the air delta P was 2.6 inches = of water across the radiator and the oil cooler cores. >=20 > After the air flow through the oil cooler was increased while leaving = the radiator air flow unchanged, the Oil T dropped from 212 to 160 deg = while the Water T dropped from 212 to 200 deg. At this time, the oil = cooler oil delta T was 33 deg and the radiator water delta T was 15 = deg. >=20 > My conclusion from this is that it will be difficult to cause a = significant change in the coolant operating temperature by making = changes to the oil cooling part of the system. In real life, I was a = scientist. It may be useful to run this conclusion past an engineer. = Scientists just collect data while engineers figure out what the data = means and how make use of it. >=20 > =46rom the photo of the front of the radiator inlet duct, comparing = the inlet to the prop flange, it would appear that the duct inlet has an = area of around 27 sq in. Your previous information indicates an inlet = area of 16.5 sq in which may be the area of the inlet through the cowl. = What sort of interface do you have between the cowl and duct? >=20 > Steve Boese > RV6A, 1986 13B NA, RD1A, EC2 >=20 > From: Rotary motors in aircraft on = behalf of Stephen Izett = stephen.izett@gmail.com > Sent: Friday, December 29, 2017 12:42:29 AM > To: Rotary motors in aircraft > Subject: [FlyRotary] Re: Cooling Issues > =20 > Hi Lynn > Current testing is stationary. >=20 > I have had it on the apron doing figure 8=E2=80=99s and it seemed to = not overheat.=20 > Still to hot though. >=20 > Once its moving it seems to help with airflow. >=20 > I=E2=80=99m not going to give up on our setup just yet. > I=E2=80=99ve got a few ideas and a bunch of testing and then maybe fly = it and see what it does with some wind in its face. >=20 > What delta T=E2=80=99s should I expect from the oiling water coolers? > Sounds like 15F on the water and a fair bit more on the oil? >=20 > Cheers >=20 > Steve Izett > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html