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Bond [772]
2 years ago
9

A shell and tube heat exchanger must be designed to heat 2.5 kg/s water from 15 to 85 degrees celsius. The heating is to be acco

mplished by passing hot engine oil, which is available at 160 degrees celsius, through the shell side of the exchanger. The oil is known to provide an average convection coefficient of h0 = 400 W/mK on the outside of the tubes. Ten tubes pass the water through the shell. Each tube is thin-walled, of diameter D = 25 mm, and makes eight passes through the shell.
If the oil leaves the exchanger at 100 degrees celsius, what is its flow rate? How long must the tubes be to accomplish the desired heating?
Engineering
1 answer:
Alexus [3.1K]2 years ago
3 0

Answer:

a) \dot m_{o} = 6.105\,\frac{kg}{s}, b) L_{tube,total} = 29.144\,m

Explanation:

a) The heat transfer rate needed to heat water is:

\dot Q_{in} = \dot m_{w} \cdot c_{p,w}\cdot \Delta T_{w}

\dot Q_{in} = (2.5\,\frac{kg}{s} )\cdot (4186\,\frac{J}{kg\cdot ^{\textdegree}C} )\cdot (85^{\textdegree} C-15^{\textdegree} C)

\dot Q_{in} = 732550\,W

The mass flow rate of oil is:

\dot m_{o} = -\frac{\dot Q_{in}}{c_{p,o}\cdot \Delta T_{o}}

\dot m_{o} = - \frac{732550\,W}{\left(2000\,\frac{J}{kg\cdot ^{\textdegree}C} \right)\cdot \left (100^{\textdegree}C-160^{\textdegree}C \right)}

\dot m_{o} = 6.105\,\frac{kg}{s}

b) The formula for outer convection is:

\dot Q_{in} = h_{o}\cdot A_{s} \cdot (\overline T_{o}-\overline T_{w})

Mean temperatures are, respectively:

\overline T_{o} = \frac{160^{\textdegree}C + 100^{\textdegree}C}{2}

\overline T_{o} = 130^{\textdegree}C

\overline T_{w} = \frac{15^{\textdegree}C + 85^{\textdegree}C}{2}

\overline T_{w} = 50^{\textdegree}C

The required area is cleared in the convection equation:

A_{s} = \frac{\dot Q_{in}}{h_{o}\cdot \left(\overline T_{o}-\overline T_{w}\right)}

A_{s} = \frac{732550\,W}{\left(400\,\frac{W}{m^{2}\cdot ^{\textdegree} C} \right)\cdot (130^{\textdegree}C-50^{\textdegree}C)}

A_{s} = 22.892\,m^{2}

Last result is also given by this expression, whose length is cleared:

A_{s} = \pi \cdot D \cdot n_{tubes} \cdot n_{pass}\cdot L_{tube,unit}

L_{tube,unit} = \frac{A_{s}}{\pi \cdot D \cdot n_{tubes}\cdot n_{pass}}

L_{tube,unit} = \frac{22.892\,m^{2}}{\pi \cdot (0.025\,m)\cdot (10)\cdot (8)}

L_{tube,unit} \approx 3.643\,m

Total length of each tube is:

L_{tube, total} = 8 \cdot (3.643\,m)

L_{tube,total} = 29.144\,m

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attashe74 [19]

Answer:

a) ∀y∃x(Q(x, y))

b) (B(Jayhawks, W ildcats)→¬∀y(L(Jayhawks, y)))

c) ∃x(B(Wildcats, x) ∧ B(x, Jayhawks))

Explanation:

a) The statement can be rewritten as "For all football teams, there exists a quarterback" which is written in logical symbols.

b) The statement is an implication and thus have a premise and a conclusion. The premise states "Jayhawks beat the Wildcats" which is translated using B(x, y). The conclusion can be rewritten as "It is not the case that Jayhawks lose to all football teams".

c) The statement is a simple conjunction which can be written as "There exists a team x such that the Wildcats beats x and x beats Jayhawks"

7 0
2 years ago
A three-phase line has an impedance of 0.4 j2.7 ohms per phase. The line feeds two balanced three-phase loads that are connected
Viktor [21]

Answer:

a. The magnitude of the line source voltage is

Vs = 4160 V

b. Total real and reactive power loss in the line is

Ploss = 12 kW

Qloss = j81 kvar

Sloss = 12 + j81 kVA

c. Real power and reactive power supplied at the sending end of the line

Ss = 540.046 + j476.95 kVA

Ps = 540.046 kW

Qs = j476.95 kvar

Explanation:

a. The magnitude of the line voltage at the source end of the line.

The voltage at the source end of the line is given by

Vs = Vload + (Total current×Zline)

Complex power of first load:

S₁ = 560.1 < cos⁻¹(0.707)

S₁ = 560.1 < 45° kVA

Complex power of second load:

S₂ = P₂×1 (unity power factor)

S₂ = 132×1

S₂ = 132 kVA

S₂ = 132 < cos⁻¹(1)

S₂ = 132 < 0° kVA

Total Complex power of load is

S = S₁ + S₂

S = 560.1 < 45° + 132 < 0°

S = 660 < 36.87° kVA

Total current is

I = S*/(3×Vload)   ( * represents conjugate)

The phase voltage of load is

Vload = 3810.5/√3

Vload = 2200 V

I = 660 < -36.87°/(3×2200)

I = 100 < -36.87° A

The phase source voltage is

Vs = Vload + (Total current×Zline)

Vs = 2200 + (100 < -36.87°)×(0.4 + j2.7)

Vs = 2401.7 < 4.58° V

The magnitude of the line source voltage is

Vs = 2401.7×√3

Vs = 4160 V

b. Total real and reactive power loss in the line.

The 3-phase real power loss is given by

Ploss = 3×R×I²

Where R is the resistance of the line.

Ploss = 3×0.4×100²

Ploss = 12000 W

Ploss = 12 kW

The 3-phase reactive power loss is given by

Qloss = 3×X×I²

Where X is the reactance of the line.

Qloss = 3×j2.7×100²

Qloss = j81000 var

Qloss = j81 kvar

Sloss = Ploss + Qloss

Sloss = 12 + j81 kVA

c. Real power and reactive power supplied at the sending end of the line

The complex power at sending end of the line is

Ss = 3×Vs×I*

Ss = 3×(2401.7 < 4.58)×(100 < 36.87°)

Ss = 540.046 + j476.95 kVA

So the sending end real power is

Ps = 540.046 kW

So the sending end reactive power is

Qs = j476.95 kvar

7 0
2 years ago
A converging-diverging nozzle is designed to operate with an exit Mach number of 1.75 . The nozzle is supplied from an air reser
Flura [38]

Answer:

a. 4.279 MPa

b. 3.198 MPa to 4.279 MPa

c. 0.939 MPa

d. Below 3.198 MPa

Explanation:

From the given parameters

M_{exit} = 1.75 MPa  

M at 1.6 MPa gives A_{exit}/A* = 1.2502

M at 1.8 MPa gives  A_{exit}/A* = 1.4390

Therefore, by interpolation, we have M_{exit} = 1.75 MPa  gives A

However, we shall use M_{exit} = 1.75 MPa and A

Similarly,

P_{exit}/P₀ = 0.1878

a) Where the nozzle is choked at the throat there is subsonic flow in the following diverging part of the nozzle. From tables, we have

A_{exit}/A* = 1.387. by interpolation M

Therefore P_{exit} = P₀ × P

Which shows that the nozzle is choked for back pressures lower than 4.279 MPa

b) Where there is a normal shock at the exit of the nozzle, we have;

M₁ = 1.75 MPa, P₁ = 0.1878 × 5 = 0.939 MPa

Where the normal shock is at M₁ = 1.75 MPa, P₂/P₁ = 3.406

Where the normal shock occurs at the nozzle exit, we have

P_b = 3.406\times 0.939 = 3.198 MPa

Where the shock occurs t the section prior to the nozzle exit from the throat, the back pressure was derived as P_b = 4.279 MPa

Therefore the back pressure value ranges from 3.198 MPa to 4.279 MPa

c) At M_{exit} = 1.75 MPa  and P

d) Where the back pressure is less than 3.198 MPa according to isentropic flow relations supersonic flow will exist at the exit plane    

8 0
2 years ago
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Arlecino [84]
A should be it or b
4 0
2 years ago
Franco is responsible for decomposing the work for a project to host a major conference. Which two things should be use to get s
expeople1 [14]

Answer:

scope statement and deliverables

Explanation:

Francisco Franco Bahamonde was a Spanish general who ruled over Spain from 1939 to 1975 as a dictator., assuming the title Caudillo.

Franco's ideology included the following consistent points:

Authoritarianism

Nationalism

National Catholicism

Militarism, conservatism

Franco is responsible for decomposing the work for a project to host a major conference.

Scope statement and deliverables should be used to get started.

4 0
2 years ago
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