Mailing List flyrotary@lancaironline.net Message #67192
From: Finn Lassen finn.lassen@verizon.net <flyrotary@lancaironline.net>
Subject: Re: [FlyRotary] Re: Ed's spreadsheet
Date: Sun, 27 Feb 2022 19:24:49 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Thanks Ed. Thing is I trust your research more than mine :)

Would have been nice if chart had numbers in the 180 - 220F range, which is where my interest is. (I thought it went to 100C.)

Not sure I understand why specific heat is not directly proportional with density. But I don't know if 50/50 antifreeze is by volume or weight.

Anyhow, looks like I don't have to worry about coolant flow.

Looking at past postings, I saw a remark about the Renesis pump apparently being more effective that the 13B pump in spite of the cheap impeller.

Perhaps that's why I'm getting better gal/min flow numbers in spite of my estimated collective 0.4 sq in restriction (2 x 0.5" ID) in spite of others 1" ID 0.8 sq in hose installations.

I guess I should have posted spreadsheets showing gal/min for different RPMs rather than my inches of H2O head on pitot/static sensors. Could easily be misread by someone in the future. Has to use the WaterFlow.xls to convert measured head pressure to gal/min and entered pipe area is critical.

Finn

On 2/27/2022 11:19 AM, eanderson@carolina.rr.com wrote:

Well Looking at the chart you referernced it looks like the mixture for 50/50 the CP could range from 0.79 at -30F to 088 at 100F.  IF 100 % glyco then at -10F we have a CP of 0.53 and at 100 0f 0.66.  So looks like I picked a worst/best case condition.  But, using your example I get a cp of 0.8807.  Not a 30% difference but more than 5%


In any case, I would suggest if you find data you feel  more confident in, do not hesitate to subsitute it.

Ed

pecific Heat of Ethylene Glycol based Water Solutions

Specific Heat - cp - of ethylene glycol based water solutions at various temperatures are indicated below

Specific Heat - cp (Btu/lb oF) 
Ethylene Glycol Solution
(% by weight)
Temperature (°C) 
-50 -40 -30 -20 -10 0 10 20 30 40 50 60 70 80 90 100
0




1.0038 1.0018 1.0004 0.99943 0.99902 0.99913 0.99978 1.0009 1.0026 10049 1.0076
10




0.97236 0.97422 0.97619 0.97827 0.98047 0.98279 0.98521 0.98776 0.99041 0.99318 0.99607
20




0.93576 0.93976 0.94375 0.94775 0.95175 0.95574 0.95974 0.96373 0.96773 0.97173 0.97572
30



0.89373 0.89889 0.90405 0.90920 0.91436 0.91951 0.92467 0.92982 0.93498 0.94013 0.94529 0.95044
40


0.84605 0.85232 0.85858 0.86484 087111 0.87737 0.88364 0.88990 0.89616 0.90243 0.90869 0.91496 0.92122
50

0.79288 0.80021 0.80753 0.81485 0.82217 0.82949 0.83682 0.84414 0.85146 0.85878 0.86610 0.87343 0.88075 0.88807
60 0.72603 0.73436 0.74269 0.75102 0.75935 0.76768 0.77601 0.78434 0.79267 0.80100 0.80933 0.81766 0.82599 0.83431 0.84264 0.85097
70 0.67064 0.67992 0.68921 0.69850 0.70778 0.71707 0.72636 073564 0.74493 0.75422 0.76350 0.77279 0.78207 0.79136 0.80065 0.80993
80 0.61208 0.62227 0.63246 0.64265 0.65285 0.66304 0.67323 0.68343 0.69362 0.70381 0.71401 0.72420 0.73439 0.74458 0.75478 0.76497
90


0.58347 0.59452 0.60557 0.61662 0.62767 0.63872 0.64977 0.66082 0.67186 0.68291 0.69396 0.70501 0.71606
100



0.53282 0.54467 0.55652 0.56838 0.58023 0.59209 0.60394 0.61579 0.62765 0.63950 0.65136 0.66321
I'm not sure how
------ Original Message ------
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: 2/26/2022 9:29:22 PM
Subject: [FlyRotary] Re: Ed's spreadsheet

From your 24 Aug 2012 post about cooling section in the spreadsheet:
"Cooling mass flow is dependent on:
1. A  0.7 cp compared to pure water of 1.0 Cp - this compensates for the typical anitfreeze dilution of the specific heat of water. "

Roughly weighing a 1 Gal 50/50 antifreeze jug I get maybe 7.9 pounds after subtracting 0.3 pound for the jug). Pure water about 8.3 pounds. That's about 5%.
I realize it changes somewhat with temperature but nowhere near 30% ?

https://www.engineeringtoolbox.com/ethylene-glycol-d_146.html

Difference between water and 50/50 at 100C: 1000/1030 or 3%. Not 30%.

Difference in specific heat (whatever that is): 1.0079 / 0.88807 = 13% (for 50/50 at 100C).

What am I missing?

Finn

On 2/26/2022 10:48 AM, eanderson@carolina.rr.com wrote:

I agree, must have got it from someplace credible - like Bill Shertz.
CP was 1.0 for pure H20 and somewhat less with antifreeze mixed in.
I had a primary pully from MazdaTrix that reduced water pump speed - since engine was turning faster than normal in automobile, did not want to have any cavitation.  So my water pump did turn a bit slower than stock.
Not necessarily - note that water flow drops off if pump speed increases into the "caviation range"


------ Original Message ------
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: 2/25/2022 10:39:43 AM
Subject: [FlyRotary] Re: Ed's spreadsheet

Thanks Ed.

But 185.85 seems pretty detailed for a SWAG.
Any chance you got it from Bill Shertz's tests (which I unfortunately can't find the posts about)?

What determines "Cp Coolant"?
Heat transfer efficiency from engine to water and water to rad?

From measuring the rims of the e-shaft pulley (122mm) and water pump pulley (112mm) it looks like the Renesis water pump runs a bit slower (factor 1.09 compared to your 1.18).

Should water flow be directly proportional to water pump RPM?

Finn

On 2/25/2022 10:07 AM, eanderson@carolina.rr.com wrote:
Sorry, Finn.

Too much water under the bridge, pretty sure I did not make it up out of thin air.  I suspect I  visited some pump websites to arrive at a SWAG.

Ed

------ Original Message ------
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: 2/24/2022 2:25:56 PM
Subject: [FlyRotary] Ed's spreadsheet

Hi Ed,
 
From where did you get the 13B coolant flow numbers (Pump Factor)?
 
I want to be certain that I have adequate coolant flow.
 
Finn
 
 
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