Heat Capacity Ratio of Water at 1000°C | 1273.15K

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The discussion focuses on determining the heat capacity ratio of water at 1000°C (1273.15K), with the user struggling to find relevant data beyond 375°C. They reference the NASA polynomial databases, which provide coefficients for calculating heat capacity using a specific formula. The coefficients a1 to a5 for the high temperature range are provided, but there is confusion regarding their individual meanings. Clarification on the scientific notation used for the coefficients is also discussed. The conversation highlights the importance of accurate heat capacity data for rocket engine design.
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Hello,
I am trying to find the heat capacity ratio of water at 1000C or 1273.15K.
I have tried to find it through various website but have yet to find anything past 375C. I could find the gamma if I was given any of the two types of heat capacity ratios (volumetric or pressure) I could get it myself. I would like to find this out because it is useful for a rocket engine I am trying to design.
 
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The heat capacities are known from experiments and documented in the NASA polynomial databases, e.g. here:
http://www.me.berkeley.edu/gri-mech/data/nasa_plnm.html

There, you see that heat capacity can be calculated using
Cp/R = a1 + a2 T + a3 T^2 + a4 T^3 + a5 T^4
where the coefficients a are given in the thermodynamic database:
http://www.me.berkeley.edu/gri-mech/version30/files30/thermo30.dat

In the thermodynamic database mentioned there, the H2O entry is:
H2O L 8/89H 2O 1 G 200.000 3500.000 1000.000 1
3.03399249E+00 2.17691804E-03-1.64072518E-07-9.70419870E-11 1.68200992E-14 2
-3.00042971E+04 4.96677010E+00 4.19864056E+00-2.03643410E-03 6.52040211E-06 3
-5.48797062E-09 1.77197817E-12-3.02937267E+04-8.49032208E-01 4

the coefficients a1..a5 for the high temperature range 1000 K - 3500 K are given in line 2
 
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bigfooted said:
The heat capacities are known from experiments and documented in the NASA polynomial databases, e.g. here:
http://www.me.berkeley.edu/gri-mech/data/nasa_plnm.html

There, you see that heat capacity can be calculated using
Cp/R = a1 + a2 T + a3 T^2 + a4 T^3 + a5 T^4
where the coefficients a are given in the thermodynamic database:
http://www.me.berkeley.edu/gri-mech/version30/files30/thermo30.dat

In the thermodynamic database mentioned there, the H2O entry is:
H2O L 8/89H 2O 1 G 200.000 3500.000 1000.000 1
3.03399249E+00 2.17691804E-03-1.64072518E-07-9.70419870E-11 1.68200992E-14 2
-3.00042971E+04 4.96677010E+00 4.19864056E+00-2.03643410E-03 6.52040211E-06 3
-5.48797062E-09 1.77197817E-12-3.02937267E+04-8.49032208E-01 4

the coefficients a1..a5 for the high temperature range 1000 K - 3500 K are given in line 2

Thank you for the help bigfooted but I am sorry to say that I don't really understand the differences in the different a# coeffficients. I understand what to do with them but do not really know which a is which
 
dbmorpher said:
Thank you for the help bigfooted but I am sorry to say that I don't really understand the differences in the different a# coeffficients. I understand what to do with them but do not really know which a is which

a1=3.03399249E+00
a2=2.17691804E-03
a3=-1.64072518E-07
a4=9.70419870E-11
a5=1.68200992E-14

You are familiar with E format for representing powers of 10, correct?
 
Yes I am Chestermiller thank you for clarifying the constants for me.
 
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