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blondinia [14]
3 years ago
10

Determine the maximum height (in inches) that a lift pump can raise water (0.9971 g/ml) from a well at normal atmospheric pressu

re. Also present the cancellation of units to arrive at the final unit? Pls help. with solution​
Engineering
1 answer:
solniwko [45]3 years ago
7 0

Answer:Height = 30 inches​

Mass of water / Volume of water x Gravity constant for Earth x Density of Water. This cancels out to give us mass/volume, which is then cancelling mass, giving us the final unit of length/area (in this case inches).​

Explanation:

Height = 30 inches.

Units cancelled:

30/30 x 9.8 x 0.9971 = 30/39.97

The final units are in inches!​

2. Determine the weight (in pounds) that an ice cube at 32°F will displace when placed in water at 75°F.

Weight of ice cube / Volume of water x Gravity constant for Earth x Density of Ice = Weight displaced by ice cube in pounds​

Weight of ice cube / Volume of water x Gravity constant for Earth x Density of Ice = 0.5/75 x 32 x 0.92 = 0.5/22.67

The final units are in pounds!​

3. Determine the mass (in grams) of an ice cube at 32°F when placed in water at 75°F (assume no change in volume).

Mass of Ice Cube / Volume of Water x Gravity constant for Earth x Density of Ice = Mass of ice cube in grams

Mass of Ice Cube / Volume of Water x Gravity constant for Earth x Density of Ice = 0.5/75 x 32 x 0.92 = 15/22.67

The final units are in grams!​

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Explanation:

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Deviations from the engineering drawing cannot be made without the approval of the
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a. contractor

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Both portions of the rod ABC are made of an aluminum for whichE = 70 GPa. Knowing that the magnitude of P is 4 kN, determine(a)
san4es73 [151]

Explanation:

ΔL_{BC} = ΔL_{AB}

\frac{(Q - 4000)(0.5)}{3.14* 0.03 *0.03 *70*10^{9} }     (1)

= \frac{4000*0.4}{3.14*0.01*0.01*70*10^{9} }

Q = 32,800 N

now put this value in equation 1.

Deflection of B = \frac{(32800-4000)(0.5)}{3.14*0.03*0.03*70*10^{9} }

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4 0
4 years ago
An air-standard dual cycle has a compression ratio of 9.1 and displacement of Vd = 2.2 L. At the beginning of compression, p1 =
jok3333 [9.3K]

Answer:

a) T₂ is 701.479 K

T₃ is 1226.05 K

T₄ is 2350.34 K

T₅ is 1260.56 K

b) The net work of the cycle in kJ is 2.28 kJ

c) The power developed is 114.2 kW

d) The thermal efficiency, \eta _{dual} is 53.78%

e) The mean effective pressure is 1038.25 kPa

Explanation:

a) Here we have;

\frac{T_{2}}{T_{1}}=\left (\frac{v_{1}}{v_{2}}  \right )^{\gamma -1} = \left (r  \right )^{\gamma -1} = \left (\frac{p_{2}}{p_{1}}  \right )^{\frac{\gamma -1}{\gamma }}

Where:

p₁ = Initial pressure = 95 kPa

p₂ = Final pressure =

T₁ = Initial temperature = 290 K

T₂ = Final temperature

v₁ = Initial volume

v₂ = Final volume

v_d = Displacement volume =

γ = Ratio of specific heats at constant pressure and constant volume cp/cv = 1.4 for air

r = Compression ratio = 9.1

Total heat added = 4.25 kJ

1/4 × Total heat added = c_v \times (T_3 - T_2)

3/4 × Total heat added = c_p \times (T_4 - T_3)

c_v = Specific heat at constant volume = 0.718×2.821× 10⁻³

c_p = Specific heat at constant pressure = 1.005×2.821× 10⁻³

v₁ - v₂ = 2.2 L

\left \frac{v_{1}}{v_{2}}  \right =r  \right = 9.1

v₁ = v₂·9.1

∴ 9.1·v₂ - v₂ = 2.2 L  = 2.2 × 10⁻³ m³

8.1·v₂ = 2.2 × 10⁻³ m³

v₂ = 2.2 × 10⁻³ m³ ÷ 8.1 = 2.72 × 10⁻⁴ m³

v₁ = v₂×9.1 = 2.72 × 10⁻⁴ m³ × 9.1 = 2.47 × 10⁻³ m³

Plugging in the values, we have;

{T_{2}}= T_{1} \times \left (r  \right )^{\gamma -1}  = 290 \times 9.1^{1.4 - 1} = 701.479 \, K

From;

\left (\frac{p_{2}}{p_{1}}  \right )^{\frac{\gamma -1}{\gamma }}= \left (r  \right )^{\gamma -1} we have;

p_{2} = p_{1}} \times \left (r  \right )^{\gamma } = 95 \times \left (9.1  \right )^{1.4} = 2091.13 \ kPa

1/4×4.25 =  0.718 \times 2.821 \times  10^{-3}\times (T_3 - 701.479)

∴ T₃ = 1226.05 K

Also;

3/4 × Total heat added = c_p \times (T_4 - T_3) gives;

3/4 × 4.25 = 1.005 \times 2.821 \times  10^{-3} \times (T_4 - 1226.05) gives;

T₄ = 2350.34 K

\frac{T_{4}}{T_{5}}=\left (\frac{v_{5}}{v_{4}}  \right )^{\gamma -1} = \left (\frac{r}{\rho }  \right )^{\gamma -1}

\rho = \frac{T_4}{T_3} = \frac{2350.34}{1226.04} = 1.92

T_{5} =  \frac{T_{4}}{\left (\frac{r}{\rho }  \right )^{\gamma -1}}= \frac{2350.34 }{\left (\frac{9.1}{1.92 }  \right )^{1.4-1}} =1260.56 \ K

b) Heat rejected =  c_v \times (T_5 - T_1)

Therefore \ heat \ rejected =  0.718 \times 2.821 \times  10^{-3}\times (1260.56 - 290) = 1.966 kJ

The net work done = Heat added - Heat rejected

∴ The net work done = 4.25 - 1.966 = 2.28 kJ

The net work of the cycle in kJ = 2.28 kJ

c) Power = Work done per each cycle × Number of cycles completed each second

Where we have 3000 cycles per minute, we have 3000/60 = 50 cycles per second

Hence, the power developed = 2.28 kJ/cycle × 50 cycle/second = 114.2 kW

d)

Thermal \ efficiency, \, \eta _{dual} =  \frac{Work \ done}{Heat \ supplied} = \frac{2.28}{4.25} \times 100 = 53.74 \%

The thermal efficiency, \eta _{dual} = 53.78%

e) The mean effective pressure, p_m, is found as follows;

p_m = \frac{W}{v_1 - v_2} =\frac{2.28}{2.2 \times 10^{-3}} = 1038.25 \ kPa

The mean effective pressure = 1038.25 kPa.

3 0
4 years ago
20 points and brainliest A, B, C, D
Annette [7]
B !! Is the correct answer
5 0
3 years ago
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