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.
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.
(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 gV:=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 |