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Modern Engineering Thermodynamics

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620 CHAPTER 15: Chemical <strong>Thermodynamics</strong><br />

EXAMPLE 15.11<br />

We want to measure the heat of combustion of liquid octane by burning<br />

it in the rigid, sealed, adiabatic bomb calorimeter shown in Figure 15.9.<br />

The internal volume is of the combustion bomb is 50.0 × 10 −3 ft 3 .We<br />

insert 10.0 grams of fuel and fill the bomb with enough pure oxygen to<br />

have 50.0% excess oxygen for the combustion reaction. Determine the<br />

maximum possible explosion pressure inside the bomb when the fuel is<br />

ignited.<br />

Solution<br />

The molecular mass of octane ðC 8 H 18 Þ is 114 kg/kgmole, so at 10.0 g<br />

(0.0100 kg), it contains<br />

T = T A<br />

p = p max<br />

ð0:0100 kgÞ/ ð114 kg/kgmoleÞ = 8:77 × 10 −5 kgmole<br />

The reaction equation for 50.0% excess pure oxygen is<br />

C 8 H 18 + 1:5ð12:5ÞðO 2 Þ ! 8CO ð 2 Þ+ 9H ð 2 OÞ+ 6:25ðO 2 Þ<br />

and 8.77 × 10 −5 kgmole of octane yields<br />

or<br />

8:77 × 10 −5 ð8 + 9 + 6:25Þ = 2:00 × 10 −3 kgmole of product<br />

FIGURE 15.9<br />

Example 15.11.<br />

2:00 × 10 −3 kgmole ð2:2046 lbmole/kgmoleÞ = 4:41 × 10 −3 lbmole of product<br />

We can estimate the adiabatic flame temperature for this closed system reaction from Eq. (15.18) using the temperatureaveraged<br />

molar constant volume specific heats found in Table 15.6:<br />

<br />

T A closed<br />

system<br />

= T°+<br />

h f ° fuel −∑ R<br />

ðn i /n fuel<br />

∑<br />

P<br />

ÞRT° −∑<br />

R<br />

ðn i /n fuel Þðc vi<br />

ðn i /n fuel Þðh° f − RT°Þ i<br />

Þ avg<br />

Since the fuel is in liquid form at a low pressure here, we use the approximation ðu f Þ fuel ≈ h f ° fuel : Since<br />

RT° =ð0:0083143Þð298:15Þ = 2:4789 MJ/kgmole is a constant, the numerator of Eq. (15.18) becomes<br />

and the denominator is<br />

Then, Eq. (15.18) gives<br />

and Eq. (15.19) gives<br />

P max = n pRT A<br />

V p<br />

− 249:952 − 1:5ð12:5Þð2:4789Þ− 8ð−393:522 − 2:4789Þ<br />

− 9ð−241:827 − 2:4789Þ− 6:25ð0 − 2:4789Þ = 5090 MJ<br />

8ð0:04987Þ + 9ð0:03419Þ + 6:25ð0:02468Þ = 0:861 MJ/K<br />

ðT A Þ bomb = 25:0 + 5090 = 5930°C = 6210 K = 11,200 R<br />

calorimeter 0:861<br />

ð<br />

= 4:41 × 10−3 lbmoleÞ 1545:35 ft . lbf/ ðlbmole . RÞ ð11:2 × 10 3 RÞ<br />

50:0 × 10 − 3 ft 3 144 in 2 /ft<br />

2 = 10,600 psi<br />

Exercises<br />

31. Determine the maximum explosion pressure in Example 15.11 for a bomb volume of 10.0 × 10 −3 ft 3 instead of 50.0 ×<br />

10 −3 ft 3 . Assume all the remaining variables are unchanged. Answer: p max explosion = 53,900 psi.<br />

32. If the amount of fuel used in the bomb calorimeter in Example 15.11 is 50.0 grams instead of 10.0 grams, determine<br />

the maximum explosion pressure in the bomb. Assume all the remaining variables are unchanged.<br />

Answer: p max explosion = 53,900 psi.<br />

33. If the bomb calorimeter in Example 15.11 is filled with 100.% excess oxygen instead of 50.0% excess oxygen, determine<br />

the maximum explosion pressure in the bomb. Assume all the remaining variables are unchanged.<br />

Answer: p max explosion = 11,700 psi.

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