Question 1.38: A 300-ft^3 oxygen tank is compressed under a pressure of 500...

A 300-ft^{3} oxygen tank is compressed under a pressure of 500 psia and at a temperature of 40^{\circ }F . (a) Determine the density of the oxygen in the tank. (b) Determine the weight of the oxygen in the tank.

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(a) To determine the density of the oxygen in the tank, one may apply either Equation 1.104 p=\rho RT or Equation 1.117 pV=NR_{u} T. Equation 1.104 is applied in this Example Problem as follows:
p=\rho RT
where the gas constant, R for oxygen is read from Table A.5 in Appendix A as follows:

slug:=1lb\frac{sec^{2} }{ft}                 P:=500psi=7.2\times 10^{4} psf

T:=40^{\circ } =499.67^{\circ } R                R:=1554\frac{ft lb}{slug^{\circ } R}

Guess value:                          \rho :=1\frac{slug}{ft^{3} }

Given

P=\rho RT
\rho :=Find (\rho )0.093\frac{slug}{ft^{3} }

(b) To determine the weight of the oxygen in the tank, Equation 1.44 \gamma =\frac{W}{V}=\frac{Mg}{V}=\rho g is applied as follows:

\gamma =\frac{W}{V}=\frac{Mg}{V}=\rho g

V:=300ft^{3}                 g:=32.2\frac{ft}{sec^{2} }

\gamma :=\rho         g=2.991 \frac{lb}{ft^{3} }                 W:=\gamma V=897.385lb

Table A.5
Physical Properties for Some Common Gases at Standard Sea-Level Atmospheric Pressure at Room Temperature (68^{\circ } or 20^{\circ }C )
Gas
at 68^{\circ }
Chemical
Formula
Molar Mass
(m)
slug=slug-
mol
Density
(ρ)
slug/ft^{3}
Absolute (Dynamic)
Viscosity
(μ)
10^{-6} Ib-sec/ft^{2}
Gas
Constant
(R)
ft-Ib/(slug-^{\circ }R )=ft^{2}/(sec^{2} -^{\circ }R )
Specific Heat Specific Heat
Ratio,
K=C_{\rho }/C_{\upsilon }
C_{\rho } C_{\upsilon }
ft-Ib/(slug-^{\circ }R )=ft^{2}/(sec^{2} -^{\circ }R )
Air 28.960 0.002310 0.376 1715 6000 4285 1.40
Carbon dioxide CO_{2} 44.010 0.003540 0.310 1123 5132 4009 1.28
Carbon monoxide CO 28.010 0.002260 0.380 1778 6218 4440 1.40
Helium He 4.003 0.000323 0.411 12.420 31.230 31.230 1.66
Hydrogen H_{2} 2.016 0.000162 0.189 24.680 86.390 86.390 1.40
Methane CH_{2} 16.040 0.001290 0.280 3100 13.400 13.400 1.30
Nitrogen N_{2} 28.020 0.002260 0.368 1773 6210 4437 1.40
Oxygen O_{2} 32.000 0.002580 0.418 1554 5437 3883 1.40
Water vapor H_{2}O 18.020 0.001450 0.212 2760 11.110 8350 1.33
at 20^{\circ } C kg/kg-mol kg/m^{3} 10^{-6} N-sec/m^{2} N-m/(kg-^{\circ}K )=m^{2} /(sec^{2}-^{\circ}K ) N-m/(kg-^{\circ}K )=m^{2} /(sec^{2}-^{\circ}K )
Air 28.960 1.2050 18.0 287 1003 716 1.40
Carbon dioxide CO_{2} 44.010 1.8400 14.8 188 858 670 1.28
Carbon monoxide CO 28.010 1.1600 18.2 297 1040 743 1.40
Helium He 4.003 0.1660 19.7 2077 5220 3143 1.66
Hydrogen H_{2} 2.016 0.0839 9.0 4120 14.450 10.330 1.40
Methane CH_{2} 16.040 0.6680 13.4 520 2250 1730 1.30
Nitrogen N_{2} 28.020 1.1600 17.6 297 1040 743 1.40
Oxygen O_{2} 32.000 1.3300 20.0 260 909 649 1.40
Water vapor H_{2}O 18.020 0.7470 10.1 462 1862 1400 1.33

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