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Gnom [1K]
4 years ago
13

To reduce the drag coefficient and thus to improve the fuel efficiency, the frontal area of a car is to be reduced. Determine th

e amount of fuel and money saved per year as a result of reducing the frontal area from 20 to 13 ft2 . Assume the car is driven 12,000 mi a year at an average speed of 55 mi/h. Take the density and price of gasoline to be 50 lbm/ft3 and $3.10/gal, respectively; the density of air to be 0.075 lbm/ft3 , the heating value of gasoline to be 20,000 Btu/lbm; and the overall efficiency of the drive train to be 30 percent.
Engineering
1 answer:
Alex787 [66]4 years ago
8 0

Answer:

Amount reduction is 29.06 gal/year

Cost of reduction is $90.09 / year

Explanation:

Assume The effect of reduction of the frontal area on the drag coefficient is

negligible

Given that:

The drag coefficient (C_D) = 0.4 for a passenger car.

A = frontal area of car = 18 ft²

Velocity (V) = 55 mile per hour = (55 × 1.4667) ft/s = 80.6685 ft/s, density of air (ρ) = 0.075 lbm/ft³

The frontal drag force can be calculated by:

F_D=C_DA\frac{\rho V^2}{2} =0.3 *18*\frac{0.075*80.6685^2}{2} =1317.75\\F_D=1317.75lbm.ft/s^2=(1317,75*\frac{1}{32.2})lbf=40.9lbf

The amount of work done to overcome this drag force is calculated by:

d = 12000 miles per year

W_{DRAG}=F_D*d=(40.9lbf)*(12000miles/year)*\frac{5280ft}{1mile}*\frac{1lbf}{778.169 lbf ft}  =3.330* 10^6 Btu/year

and the required energy  input is:

E_{in}=\frac{W_{DRAG}}{\eta_{car}} =\frac{3.330*10^6Btu/year}{0.30} =11.1*10^7Btu/year

Heating value (HV) = 20000 Btu/lbm

m_{fuel}=E_{in}/HV=1.11*10^7/20000\\

Amount of fuel = \frac{m_{fuel}}{\rho{fuel}} = \frac{1.11*10^7/20000}{50}=11.1ft^3/year *\frac{7.4804gal}{1ft^3}=83.03 gal/year

Cost of fuel = Amount of fuel × Price of fuel = 11.1 ft³/year × ($3.1/gal) × (7.4804 gal / 1 ft³) = $257.4 per year.

The percent  reduction in the fuel consumption due to reducing frontal area (reduction ratio) is given by:

Reduction ratio = \frac{A-A{new}}{A}=\frac{20-13}{20}  =0.35

Amount reduction = Reduction ratio × Amount of fuel = 0.35 × 83.03 gal/year =29.06 gal/year

Cost of reduction = Reduction ratio × cost of fuel = 0.35 × $257.4 = $90.09 / year

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Calculate the energy in kJ added to 1 ft3 of water by heating it from 70° to 200°F.
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Answer:

The energy in kJ is 8558.16 kJ.

Explanation:

Data presented in the problem:

Water is heated from 70 (T1) to 200 °F (T2).

Volume (V) of the water is 1 ft3.

It is required for the specific heat of water(HW), which is 1 BTU/lb°F.

First, we need to calculate the mass of water (M) presented in the process. Water density (D) is 62. 4 lb/ft3.

M = V*D = (1ft3)*(62.4 lb/ft3) = 62.4 lb Water.

.After that, we can calculate the heat required (Q).

Q = M*HW*(T2 - T1) = (62.4 lb)*(1 BTU/lb°F)(200 °F - 70°F)

Q = 62.4 * 130 BTU = 8112 BTU.

Q is converted to kJ units using the conversion factor 1 BTU = 1.055 kJ

Q = 8112 BTU * (1.055 kJ/1BTU) = 8558.16 kJ.

Finally, the energy required is 8558.16 kJ.

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What is the maximum number of 12-2 with ground nonmetallic-sheathed cables permitted in an 18-cubic-inch device box if two singl
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The coefficient of performance of a reversible refrigeration cycle is always (a) greater than, (b) less than, (c) equal to the c
bezimeni [28]

Answer:

Option B is correct

Explanation:

Let

Higher temperature = T_H

Lower temperature = T_L

We know that COP is given by

COP = \frac{T_L}{T_H-T_L}

We see that COP is depends only on the temperature difference & Temperature difference is maximum for the Carnot cycle.

Therefore the COP of reversible refrigeration cycle is always less then the COP of  an irreversible refrigeration cycle when each operates between the same two thermal reservoirs.

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Answer:

q=4.013\:\:kW\\\\T_1=278.91\:\:^{\circ}C\\\\T_2=275.82\:\:^{\circ}C

Explanation:

R_{conv,1}=(h_1\pi D_1L)^{-1}=(50*0.25*2)^{-1}=0.01273\:\:K/W\\\\R_{conv,2}=(h^2*4wL)^{-1}=(4*4*1)^{-1}=0.0625\:\:K/W\\\\R_{cond(2D)}=(Sk)^{-1}=(8.59*150)^{-1}=0.00078\:\:K/W

So, heat rate can be calculated as follows:

q=\frac{T_{\infty,1}-T_{\infty,2}}{R_{conv,1}+R_{conv,2}+R_{cond(2D)}} =\frac{330-25}{0.076} =4.013\:\:kW

Surface temperatures can be calculated as follows:

T_1=T_{\infty,1}-qR_{conv,1}=330-51.09=278.91\:\:^{\circ}C\\\\T_2=T_{\infty,2}+qR_{conv,2}=25+250.82=275.82\:\:^{\circ}C

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