Mailing List flyrotary@lancaironline.net Message #67190
From: eanderson@carolina.rr.com <flyrotary@lancaironline.net>
Subject: Re: [FlyRotary] Re: Ed's spreadsheet
Date: Sun, 27 Feb 2022 16:19:51 +0000
To: Rotary motors in aircraft <flyrotary@lancaironline.net>

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 0.88 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) 
-50-40-30-20-100102030405060708090100
01.00381.00181.00040.999430.999020.999130.999781.00091.00261.00491.0076
100.972360.974220.976190.978270.980470.982790.985210.987760.990410.993180.99607
200.935760.939760.943750.947750.951750.955740.959740.963730.967730.971730.97572
300.893730.898890.904050.909200.914360.919510.924670.929820.934980.940130.945290.95044
400.846050.852320.858580.864840.871110.877370.883640.889900.896160.902430.908690.914960.92122
500.792880.800210.807530.814850.822170.829490.836820.844140.851460.858780.866100.873430.880750.88807
600.726030.734360.742690.751020.759350.767680.776010.784340.792670.801000.809330.817660.825990.834310.842640.85097
700.670640.679920.689210.698500.707780.717070.726360.735640.744930.754220.763500.772790.782070.791360.800650.80993
800.612080.622270.632460.642650.652850.663040.673230.683430.693620.703810.714010.724200.734390.744580.754780.76497
900.583470.594520.605570.616620.627670.638720.649770.660820.671860.682910.693960.705010.71606
1000.532820.544670.556520.568380.580230.592090.603940.615790.627650.639500.651360.66321
    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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