This value is of particular importance in waste heat work and it is regrettable that there is such a variation in the different experiments. Mallard and Le Chatelier determined values considerably higher than any given in [Table 28] . All things considered in view of the discrepancy of the values given, there appears to be as much ground for the use of a constant value for the specific heat of air at any temperature as for a variable value. Where this value is used throughout this book, it has been taken as 0.24.

Air may carry a considerable quantity of water vapor, which is frequently 3 per cent of the total weight. This fact is of importance in problems relating to heating drying and the compressing of air. [Table 29] gives the amount of vapor required to saturate air at different temperatures, its weight, expansive force, etc., and contains sufficient information for solving practically all problems of this sort that may arise.

[Pg 149]

[TABLE 29]
WEIGHTS OF AIR, VAPOR OF WATER, AND SATURATED MIXTURES OF AIR AND VAPOR
AT DIFFERENT TEMPERATURES,
UNDER THE ORDINARY ATMOSPHERIC PRESSURE OF 29.921 INCHES OF MERCURY
Temper-
ature Degrees Fahr-
enheit
Volume of Dry Air at Different Temper-
atures, the Volume at 32 Degrees being 1.000
Weight of Cubic Foot of Dry Air at the Different Temper-
atures Pounds
Elastic Force of Vapor in Inches of Mercury (Regnault)Mixtures of Air Saturated with VaporCubic Feet of Vapor from One Pound of Water at its own Pressure in Column 4
Elastic Force of the Air in the Mixture of Air and Vapor in Inches of MercuryWeight of Cubic Foot of the Mixture of Air and VaporWeight of Vapor Mixed with One Pound of Air, in PoundsWeight of Dry Air Mixed with One Pound of Vapor, in Pounds
Weight of the Air in PoundsWeight of the Vapor in PoundsTotal Weight of Mixture in Pounds
1 2 3 4 5 6 7 8 91011
0 .935.0864 .04429.877.0863.000079.086379 .000921092.4
12 .960.0842 .07429.849.0840.000130.084130 .00155 646.1
22 .980.0824 .11829.803.0821.000202.082302 .00245 406.4
321.000.0807 .18129.740.0802.000304.080504 .00379 263.81 3289
421.020.0791 .26729.654.0784.000440.078840 .00561 178.18 2252
521.041.0776 .38829.533.0766.000627.077227 .00810 122.17 1595
621.061.0761 .55629.365.0747.000881.075581 .01179 84.79 1135
721.082.0747 .78529.136.0727.001221.073921 .01680 59.54 819
821.102.0733 1.09228.829.0706.001667.072267 .02361 42.35 600
921.122.0720 1.50128.420.0684.002250.070717 .03289 30.40 444
1021.143.0707 2.03627.885.0659.002997.068897 .04547 21.98 334
1121.163.0694 2.73127.190.0631.003946.067046 .06253 15.99 253
1221.184.0682 3.62126.300.0599.005142.065042 .08584 11.65 194
1321.204.0671 4.75225.169.0564.006639.063039 .11771 8.49 151
1421.224.0660 6.16523.756.0524.008473.060873 .16170 6.18 118
1521.245.0649 7.93021.991.0477.010716.058416 .22465 4.45 93.3
1621.265.063810.09919.822.0423.013415.055715 .31713 3.15 74.5
1721.285.062812.75817.163.0360.016682.052682 .46338 2.16 59.2
1821.306.061815.96013.961.0288.020536.049336 .71300 1.402 48.6
1921.326.060919.82810.093.0205.025142.0456421.22643 .815 39.8
2021.347.060024.450 5.471.0109.030545.0414452.80230 .357 32.7
2121.367.059129.921 0.000.0000.036820.036820Infinite .000 27.1

Column 5 = barometer pressure of 29.921, minus the proportion of this due to vapor pressure from column 4.

[Pg 150]

COMBUSTION

Combustion may be defined as the rapid chemical combination of oxygen with carbon, hydrogen and sulphur, accompanied by the diffusion of heat and light. That portion of the substance thus combined with the oxygen is called combustible. As used in steam engineering practice, however, the term combustible is applied to that portion of the fuel which is dry and free from ash, thus including both oxygen and nitrogen which may be constituents of the fuel, though not in the true sense of the term combustible.

Combustion is perfect when the combustible unites with the greatest possible amount of oxygen, as when one atom of carbon unites with two atoms of oxygen to form carbon dioxide, CO2. The combustion is imperfect when complete oxidation of the combustible does not occur, or where the combustible does not unite with the maximum amount of oxygen, as when one atom of carbon unites with one atom of oxygen to form carbon monoxide, CO, which may be further burned to carbon dioxide.

Kindling Point—Before a combustible can unite with oxygen and combustion takes place, its temperature must first be raised to the ignition or kindling point, and a sufficient time must be allowed for the completion of the combustion before the temperature of the gases is lowered below that point. [Table 30], by Stromeyer, gives the approximate kindling temperatures of different fuels.