Mailing List flyrotary@lancaironline.net Message #4057
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Bill Eslick Radiator coolant delta T
Date: Tue, 21 Oct 2003 17:39:28 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
----- Original Message -----
Sent: Tuesday, October 21, 2003 1:18 PM
Subject: [FlyRotary] Re: Radiator coolant delta T

I promised to report my indicated water temps next chance I got. Here are some samples:
 
OAT(F)        Delta T (F)
69                    23
66                    19
68                    10
75                    14   
65                    15
75                    7
77                    12
 
All figures are in cruise at 8,000 to 10,000 MSL.  Last reading was in climbout, but not much difference.  I really can't explain the range of readings, but that is what it read!
 
 
Thanks for the data, Bill
 
  I ran it through my model, but did not have your power or fuel burn or airspeed.  But assuming you were doing approx 140 Indictated air speed at altitude and modest power (5200 rpm) my figures shows a delta T of 12.27F.  If you were running a bit harder the delta T would go up a bit.  If you were moving faster than 140 indicated at 5200 rpm then it would go down a bit.
 
For climb I assumed 120 Indicated and a minimum of 130HP this gave me a delta T of 24F for the radiators.  Both figures not too far off from what you are reporting.
 
So the delta T would seem to be dependent on your power setting and air speed most of all.  The more BTUs of heat you reject into the same amount of mass flow, the greater the delta T. However, the faster you go the more cooling mass flow you get which appears to help to hold down the delta T. 
 
In any case, appreciate the data
 
Ed Anderson
 
____________________________________________________
  IncrediMail - Email has finally evolved - Click Here
Image
IMSTP.gif
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster