X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [66.219.56.248] (HELO qnsi-xch.qnsi.net) by logan.com (CommuniGate Pro SMTP 5.1.12) with ESMTP id 2360724 for flyrotary@lancaironline.net; Sun, 30 Sep 2007 12:30:21 -0400 Received-SPF: none receiver=logan.com; client-ip=66.219.56.248; envelope-from=bhughes@qnsi.net Content-class: urn:content-classes:message Return-Receipt-To: "Bobby J. Hughes" MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----_=_NextPart_001_01C80387.EFEA1D68" Disposition-Notification-To: "Bobby J. Hughes" Subject: RE: [FlyRotary] Another cooling question X-MimeOLE: Produced By Microsoft Exchange V6.5.6944.0 Date: Sun, 30 Sep 2007 11:32:55 -0600 Message-ID: X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: [FlyRotary] Another cooling question Thread-Index: AcgDVZOs69GzKJZqQzW49BnqSjLRTgAJ5GwQ From: "Bobby J. Hughes" To: "Rotary motors in aircraft" This is a multi-part message in MIME format. ------_=_NextPart_001_01C80387.EFEA1D68 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Snip That's exactly what I HAD thought, until I was told that the air could pass through too fast and not pick up as much heat. =20 =20 Mark... this is what I was trying to communicate. It could be totally wrong so let's get more opinions. Ed?? =20 With respect to exit area size only. =20 =20 If the volume of air through the coolant radiator was moving faster than optimum the air delta T would be lower than it would be with slower air. Slower air at a higher delta T means less air needs to exit the cowl. What is optimum? Every install is unique so it needs to be viewed \ identified on each installation. Ed uses a 30% duct air speed as a reference point. If I understand this correctly the diffuser play a role in duct airspeed. If the air is not being diffused optimally the airspeed could be much higher than 30% through the part of the core. Dennis H. and I observed airspeeds through a test core at 50% + without a diffuser.=20 =20 Your inlets are 72sqin with 306sqin core face for water and 24.75 sqin with 102 sqin for oil. Both are competing for the same exit area. IF this is an exit area problem only then enlarging it should improve both water and oil proportionally. Water should realize 2/3 of the improvement and oil 1/3. 306 sqin vs 102 sqin. Your improvements after opening the exit seem to track this very close. So increasing your exit area further should show more improvements in both oil and water to a point. But you do not need more water cooling improvements right? =20 Core 306 sqin at an airspeed of 115mph. =20 40% or 46 mph =3D 8602 cfm 8602 cfm at a 50 deg air delta T =3D 7741 = btu's \ min 30% or 34.5 =3D 6451 cfm 6451 cfm at a 80 deg air delta T =3D = 7741 btu's \ min =20 In this example 2151 cfm less air needs to flow through the water radiator to produce the same btu rejection. So what effect would 2151 cfm less air through the water radiator and exit area have on the oil cooler's ability to flow more air? Would it improve the oil cooler air flow by 1/3 or 717 cfm? Not sure. =20 =20 Can your radiator produce a 80 deg air delta T? It may only produce 60, 70 or?? =20 Am I in left field here? =20 =20 =20 Bobby (flow testing new radiator ducts prototype today)=20 =20 =20 =20 =20 =20 =20 =20 =20 =20 =20 =20 ________________________________ From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Mark Steitle Sent: Sunday, September 30, 2007 4:28 AM To: Rotary motors in aircraft Subject: [FlyRotary] Another cooling question ED wrote: Mark, if you really had excess air flowing through your radiators the coolant would drop more than 4 Deg F. In fact, the more air flow the more coolant Delta T you would drop through the radiator.=20 =20 That's exactly what I HAD thought, until I was told that the air could pass through too fast and not pick up as much heat. This didn't make sense to me. Maybe I wasn't listening closely and missed the point altogether (wouldn't be the first time). =20 =20 What I DO know is that the air is flowing faster through the water radiator than the oil radiator. (I'm not sure I have the ASI's hooked up correctly, but they're both hooked up the same). I have a pitot behind each radiator hooked up to two separate ASI's. In slow cruise, say 125-130 kts, the water radiator ASI will read about 110knts and the oil ASI will read about 90 kts. The way it was behaving before I opened up the exit, it appeared that the air from the water radiator was trying to exit backwards through the oil inlet. I say this because of how high the oil temps were reading. I enlarged the cowl exit, and both the water and oil temps dropped significantly. =20 =20 The ASI's are referencing the static port for these readings; should they be referencing cowl or cabin pressure instead? Airspeeds readings seem awfully high to me. =20 =20 Mark (Going to the airport today to recalibrate temp sensors) =20 ------_=_NextPart_001_01C80387.EFEA1D68 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable
Snip
That's exactly what I HAD thought, until I = was told that=20 the air could pass through too fast and not pick up as much heat.  =
 
Mark... this is what I was trying to = communicate. It could=20 be totally wrong so let's get more opinions.  = Ed??
 
With respect to exit area size = only. =20
 
If the volume of air through the coolant = radiator was=20 moving faster than optimum the air delta T would be = lower than=20 it would be with slower air. Slower air at a higher delta T means less = air needs=20 to exit the cowl.  What is optimum? Every install is unique so = it=20 needs to be viewed \ identified on each installation. Ed uses = a 30%=20 duct air speed as a reference point. If I understand this correctly the = diffuser=20 play a role in duct airspeed. If the air is not being diffused optimally = the=20 airspeed could be much higher than 30% through the part of the core. = Dennis H.=20 and I observed airspeeds through a test core at 50% + without a = diffuser.=20
 
Your inlets are 72sqin with 306sqin = core face for=20 water and 24.75 sqin with 102 sqin for oil. Both are=20 competing for the same exit area. IF = this is=20 an exit area problem only then enlarging it should improve both water = and oil=20 proportionally. Water should realize 2/3 of the = improvement and=20 oil 1/3.  306 sqin vs 102 sqin. Your improvements after = opening the=20 exit seem to track this very close. So increasing your exit area = further=20 should show more improvements in both oil and water to a point. But you = do not=20 need more water cooling improvements right?
 
Core 306 sqin at an airspeed of = 115mph.
 
40% or 46 mph =3D 8602 cfm   8602 cfm = at a 50 deg=20 air delta T =3D 7741 btu's \ min
30% or 34.5 =3D 6451=20 cfm        6451 cfm at a 80 deg air = delta T =3D=20 7741 btu's \ min
 
In this example 2151 cfm less air needs to flow = through the=20 water radiator to produce the same btu rejection. So what effect would = 2151 cfm=20 less air through the water radiator and exit area have on the oil = cooler's=20 ability to flow more air? Would it improve the oil cooler air flow by = 1/3 or 717=20 cfm? Not sure.  
 
Can your radiator produce a 80 deg air delta T? = It may only=20 produce 60, 70 or??
 
Am I in left field here?
 
 
 
Bobby
(flow testing new radiator ducts prototype = today) 
 
 
 
 
 
 
 
 
 
 
 

From: Rotary motors in aircraft=20 [mailto:flyrotary@lancaironline.net] On Behalf Of Mark=20 Steitle
Sent: Sunday, September 30, 2007 4:28 AM
To: = Rotary=20 motors in aircraft
Subject: [FlyRotary] Another cooling=20 question

ED wrote:
<snip>
 Mark, if you really had excess air flowing through your = radiators the=20 coolant would drop more than 4 Deg F.  In fact, the more air flow = the more=20 coolant Delta T you would drop through the radiator. 
<snip>
 
That's exactly what I HAD thought, until I was told that the air = could pass=20 through too fast and not pick up as much heat.  This didn't make = sense to=20 me.  Maybe I wasn't listening closely and missed the point = altogether=20 (wouldn't be the first time). 
 
What I DO know is that the air is flowing faster through the water = radiator=20 than the oil radiator.  (I'm not sure I have the ASI's hooked up = correctly,=20 but they're both hooked up the same).  I have a pitot behind each = radiator=20 hooked up to two separate ASI's.  In slow cruise, say 125-130 kts, = the=20 water radiator ASI will read about 110knts and the oil ASI will read = about 90=20 kts.  The way it was behaving before I opened up the exit, it = appeared that=20 the air from the water radiator was trying to exit = backwards through=20 the oil inlet.  I say this because of how high the oil temps were=20 reading.  I enlarged the cowl exit, and both the water = and oil=20 temps dropped significantly. 
 
The ASI's are referencing the static port for these readings; = should they=20 be referencing cowl or cabin pressure instead?  Airspeeds readings = seem=20 awfully high to me. 
 
Mark
(Going to the airport today to recalibrate temp sensors)
 
------_=_NextPart_001_01C80387.EFEA1D68--