Answer:
a) [tex]L = 1.5[/tex]
[tex]L_q = 0.9[/tex]
[tex]W = \dfrac{1 }{8 } \, hour[/tex]
[tex]W_q = \dfrac{3}{40 } \, hour[/tex]
[tex]P = \dfrac{3}{5 }[/tex]
b) The new backacter should be recommended
c) The additional backacter should not be deployed
Explanation:
a) The required parameters are;
L = The number of customers available
[tex]L = \dfrac{\lambda }{\mu -\lambda }[/tex]
μ = Service rate
[tex]L_q[/tex] = The number of customers waiting in line
[tex]L_q = p\times L[/tex]
W = The time spent waiting including being served
[tex]W = \dfrac{1 }{\mu -\lambda }[/tex]
[tex]W_q[/tex] = The time spent waiting in line
[tex]W_q = P \times W[/tex]
P = The system utilization
[tex]P = \dfrac{\lambda }{\mu }[/tex]
From the information given;
λ = 12 trucks/hour
μ = 3 min/truck = 60/3 truck/hour = 20 truck/hour
Plugging in the above values, we have;
[tex]L = \dfrac{12 }{20 -12 } = \dfrac{12 }{8 } = 1.5[/tex]
[tex]P = \dfrac{12 }{20 } = \dfrac{3}{5 }[/tex]
[tex]L_q = \dfrac{3}{5 } \times \dfrac{3}{2 } = \dfrac{9}{10 } = 0.9[/tex]
[tex]W = \dfrac{1 }{20 -12 } = \dfrac{1 }{8 } \ hour[/tex]
[tex]W_q = \dfrac{3}{5 } \times \dfrac{1}{8 } = \dfrac{3}{40 } \, hour[/tex]
(b) The service rate with the new backacter = 1.5 minutes/truck which is thus;
μ = 60/1.5 trucks/hour = 40 trucks/hour
[tex]P = \dfrac{12 }{40 } = \dfrac{3}{10}[/tex]
[tex]W = \dfrac{1 }{40 -12 } = \dfrac{1 }{38 } \, hour[/tex]
[tex]W_q = \dfrac{3}{10 } \times \dfrac{1}{38 } = \dfrac{3}{380 } \, hour[/tex]
λ = 12 trucks/hour
Total cost = [tex]mC_s + \lambda WC_w[/tex]
m = 1
[tex]C_s[/tex] = GH¢ = 1300
[tex]C_w[/tex] = 400
Total cost with the old backacter is given as follows;
[tex]1 \times 1000 + 12 \times \dfrac{1}{8} \times 400 = \$ 1,600.00[/tex]
Total cost with the new backacter is given as follows;
[tex]1 \times 1300 + 12 \times \dfrac{1}{38} \times 400 = \$ 1,426.32[/tex]
The new backacter will reduce the total costs, therefore, the new backacter is recommended.
c)
Here μ = 3 min/ 2 trucks = 2×60/3 truck/hour = 40 truck/hour
[tex]\therefore W = \dfrac{1 }{40 -12 } = \dfrac{1 }{38 } \, hour[/tex]
Total cost with the one backacter is given as follows;
[tex]1 \times 1000 + 12 \times \dfrac{1}{8} \times 400 = \$ 1,600.00[/tex]
Total cost with two backacters is given as follows;
[tex]2 \times 1000 + 12 \times \dfrac{1}{38} \times 400 = \$ 2,126.32[/tex]
The additional backacter will increase the total costs, therefore, it should not be deployed.
A flashed steam geothermal power plant is located where underground hot water is available as saturated liquid at 700 kPa. The well head pressure is 600 kPa. The
flashed steam enters a turbine at 500 kPa and expands to 15 kPa, when it is condensed. The flow rate from the well is 29.6 kg/s. determine the power produced in
kW.
Answer:
The power produced by the turbine is 74655.936 kW.
Explanation:
A turbine is a device that operates at steady-state. Let suppose that turbine does not have heat interactions with surroundings, as well as changes in potential and kinetic energies are neglictible. Power output can be determined by First Law of Thermodynamics:
[tex]-\dot W_{out} + \dot m \cdot (h_{in}-h_{out}) = 0[/tex]
[tex]\dot W_{out} = \dot m\cdot (h_{in}-h_{out})[/tex]
Let suppose that water enters as saturated vapor and exits as saturated liquid. Specific enthalpies are, respectively:
[tex]h_{in} = 2748.1\,\frac{kJ}{kg}[/tex]
[tex]h_{out} = 225.94\,\frac{kJ}{kg}[/tex]
The power produce by the turbine is:
[tex]\dot W_{in} = \left(29.6\,\frac{kg}{s} \right)\cdot \left(2748.1\,\frac{kJ}{kg} - 225.94\,\frac{kJ}{kg} \right)[/tex]
[tex]\dot W_{in} = 74655.936\,kW[/tex]
A particle is emitted from a smoke stack with diameter of 0.05 mm. In order to determine how far downstream it travels it is important to find its terminal downward velocity. If it has a density of 1200 kg/m3, its terminal downward velocity (cm) is: (assume the drag coefficient is 24/Re and the volume of a sphere is 4/3 pi R3)
Answer: downward velocity = 6.9×10^-4 cm/s
Explanation: Given that the
Diameter of the smoke = 0.05 mm = 0.05/1000 m = 5 × 10^-5 m
Where radius r = 2.5 × 10^-5 m
Density = 1200 kg/m^3
Area of a sphere = 4πr^2
A = 4 × π× (2.5 × 10^-5)^2
A = 7.8 × 10^-9 m^2
Volume V = 4/3πr^3
V = 4/3 × π × (2.5 × 10^-5)^3
V = 6.5 × 10^-14 m^3
Since density = mass/ volume
Make mass the subject of formula
Mass = density × volume
Mass = 1200 × 6.5 × 10^-14
Mass M = 7.9 × 10^-11 kg
Using the formula
V = sqrt( 2Mg/ pCA)
Where
g = 9.81 m/s^2
M = mass = 7.9 × 10^-11 kg
p = density = 1200 kg/m3
C = drag coefficient = 24
A = area = 7.8 × 10^-9m^2
V = terminal velocity
Substitute all the parameters into the formula
V = sqrt[( 2 × 7.9×10^-11 × 9.8)/(1200 × 24 × 7.8×10^-9)]
V = sqrt[ 1.54 × 10^-9/2.25×10-4]
V = 6.9×10^-6 m/s
V = 6.9 × 10^-4 cm/s
The thrust F of a screw propeller is known to depend upon the diameter d,speed of advance \nu ,fluid density p, revolution per second N, and the coefficient of viscosity μ of the fluid. Determine the dimensions of each of the variables in terms of L,M,T,and find an expression for F in terms of these quantities
Answer:
screw thrust = ML[tex]T^{-2}[/tex]
Explanation:
thrust of a screw propeller is given by the equation = p[tex]V^{2}[/tex][tex]D^{2}[/tex] x [tex]\frac{ND}{V}[/tex]Re
where,
D is diameter
V is the fluid velocity
p is the fluid density
N is the angular speed of the screw in revolution per second
Re is the Reynolds number which is equal to puD/μ
where p is the fluid density
u is the fluid velocity, and
μ is the fluid viscosity = kg/m.s = M[tex]L^{-1}[/tex][tex]T^{-1}[/tex]
Reynolds number is dimensionless so it cancels out
The dimensions of the variables are shown below in MLT
diameter is m = L
speed is in m/s = L[tex]T^{-1}[/tex]
fluid density is in kg/[tex]m^{3}[/tex] = M[tex]L^{-3}[/tex]
N is in rad/s = L[tex]L^{-1}[/tex][tex]T^{-1}[/tex] =
If we substitute these dimensions in their respective places in the equation, we get
thrust = M[tex]L^{-3}[/tex][tex](LT^{-1}) ^{2}[/tex][tex]L^{2}[/tex][tex]\frac{T^{-1} L}{LT^{-1} }[/tex]
= M[tex]L^{-3}[/tex][tex]L^{2}[/tex][tex]T^{-2}[/tex]
screw thrust = ML[tex]T^{-2}[/tex]
This is the dimension for a force which indicates that thrust is a type of force
A 1000 mm wide steel sheet made of C35 is normalized by cold rolling 10 mm thick
deformed to 5 mm. The rollers, 600 mm in diameter, run at a peripheral speed of 0.12 m/s.
The deformation efficiency is 55%.
Find out:
a) the roller force
b) the roller torque
c) the performance on the pair of rollers.
Answer:
a. 20.265 MN
b. 0.555 MNm
c. 403.44 KW
Explanation:
Given:-
- The width ( w ) = 1000 mm
- Original thickness ( to ) = 10 mm
- Final thickness ( t ) = 5 mm
- The radius of the rollers ( R ) = 600 mm
- The peripheral speed of the roller ( v ) = 0.12
- Deformation efficiency ( ε ) = 55%
Find:-
a) the roller force ( F )
b) the roller torque ( T )
c) the performance on the pair of rollers. ( P )
Solution:-
- The process of flat rolling entails a pair of compressive forces ( F ) exerted by the rollers on the steel sheet that permanently deforms.
- The permanent deformation of sheet metal is seen as reduced thickness.
- We will assume that the compressive force ( F ) acts normal to the point of contact between rollers and metal sheet.
- The roll force ( F ) is defined as:
[tex]F =L*w*Y_a_v_g[/tex]
Where,
L: The projected length of strip under compression
Y_avg: The yielding stress of the material = 370 MPa
- The projected length of strip under compression is approximated by the following relation:
[tex]L = \sqrt{R*( t_o - t_f )} \\\\L = \sqrt{0.6*( 0.01 - 0.005 )} \\\\L = 0.05477 m[/tex]
- The Roll force ( F ) can be determined as follows:
[tex]F = (0.05477)*(1 )*(370*10^6 )\\\\F = 20.265 MN[/tex]
- The roll torque ( T ) is given by the following relation as follows:
[tex]T = \frac{L}{2} * F\\\\T = \frac{0.05477}{2} * 20.265\\\\T = 0.555 MNm[/tex]
- The rotational speed of the rollers ( N ) is determined by the following procedure:
[tex]f = \frac{v}{2\pi* R} = \frac{0.12}{2*\pi 0.6} = 0.03181818 \frac{rev}{s} \\\\N = f*60 = 1.9090 rpm[/tex]
- The power consumed by the pair of rollers ( P ) is given by:
[tex]P = \frac{2\pi * F * L * N}{e*60,000} KW \\\\P = \frac{2\pi * ( 20.265*10^6) * (0.05477) * (1.90909 ) }{60,000*0.55} KW\\\\P = 403.44 KW[/tex]
A particular Table in a relational database contains 100,000 Data Records/rows, each of which Data Record/row requires 200 bytes. A select statement returns all Data Records/rows in the Table that satisfy an equality search on an attribute. Estimate the time in milliseconds to complete the query when each of the following Indexes on that attribute is used.
A. No Index (Heap File of Data Records)
B. A Static Hash Index (with no overflow buckets/Pages). Assume the cost of applying the hash function is H, negligible.
The correct question is;
A particular table in a relational database contains 100,000 rows, each of which requires
200 bytes of memory. Estimate the time in milliseconds to to insert a new row into the
table when each of the following indices on the related attribute is used. Assume a page
size of 4K bytes and a page access time of 20 ms.
a. No index (heap file)
b. A clustered, non-integrated B+ tree index, with no node splitting
required. Assume that each index entry occupies 100 bytes. Assume that the
index is 75% occupied and the actual data pages are 100% occupied. Assume
that all matching entries are in a single page.
Answer:
A) 20 ms
B) 120 ms
Explanation:
A) Append (at the end of file). Just one IO, i.e., 20 ms
B) Now, when we assume that each entry in the index occupies 100 bytes, then an index page can thus hold 40 entries. Due to the fact that the data file occupies 5000 pages, the leaf level of the tree must contain at least 5000/40 pages which is 125 pages.
So, the number of levels in the tree (assuming page 75% occupancy in the
index) is (log_30 (125)) + 1 = 3. Now, if we assume that the index is clustered and not integrated with the data file and all matching entries are in a single
page, then 4 I/O operations and 80ms are required to retrieve all matching
records. Two additional I/O operations are required to update the leaf page
of the index and the data page. Hence, the time to do the insertion is
120ms.
If gear X turns clockwise at constant speed of 20 rpm. How does gear y turns?
Answer:
Gear Y would turn Counter-Clockwise do to the opposite force created from gear X.
Hope this helped! Have a great day!
Answer every question of this quiz
Please note: you can answer each question only once.
Which number shows the intake valve?
OK
I'd say number 4, number 3 looks like an exhaust valve
A multi-plate clutch is to transmit 12 kW at 1500 rev/min. The inner and outer radii for the plates are to be 50 mm and 100 mm respectively. The maximum axial spring force is restricted to lkN. Calculate the necessary number of pairs of surfaces if ll = 0-35 assuming constant ‘vyear. What will be the necessary axial force?
Answer:
The uniform pressure for the necessary axial force is W = 945 N
The uniform wear for the necessary axial force is W = 970.15 N
Explanation:
Solution
Given that:
r₁ = 0.1 m
r₂ = 0.05m
μ = 0.35
p = 12 N or kW
N = 1500 rpm
W = 1000 N
The angular velocity is denoted as ω= 2πN/60
Here,
ω = 2π *1500/60 = 157.07 rad/s
Now, the power transferred becomes
P = Tω this is the equation (1)
Thus
12kW = T * 157.07 rad/s
T = 76.4 N.m
Now, when we look at the uniform condition, we have what is called the torque that is frictional which acts at the frictional surface of the clutch dented as :
T = nμW R this is the equation (2)
The frictional surface of the mean radius is denoted by
R =2/3 [(r₁)³ - (r₂)³/(r₁)² - (r₂)²]
=[(0.1)³ - (0.05)³/[(0.1)² - (0.05)²]
R is =0.077 m
Now, we replace this values and put them into the equation (2)
It gives us this, 76. 4 N.m = n * 0.35* 1000 N * 0.077 m
n = 2.809 = 3
The number of pair surfaces is = 3
Secondly, we determine the uniform wear.
So, the mean radius is denoted as follows:
R = r₁ + r₂/ 2
=0.1 + 0.05/2
=0.075 m
Now, we replace the values and put it into the equation (2) formula
76. 4 N.m = n *0.35* 1000 N * 0.075 m
n= 2.91 = 3
Again, the number of pair surfaces = 3
However, for the uniform pressure with regards to the number of clutch plates is 3 we can derive the necessary axial force from the equation (2)
76. 4 N.m = 3 * 0.35 * W *0.077 m
W = 945 N
Also, for the uniform wear with regards to the number of clutch plates is 3 we can derive the necessary axial force from the equation (2)
76. 4 N.m = 3 * 0.35 * W *0.075 m
W = 970. 15 N
To find the reactance XLXLX_L of an inductor, imagine that a current I(t)=I0sin(ωt)I(t)=I0sin(ωt) , is flowing through the inductor. What is the voltage V(t)V(t)V(t) across this inductor?
Answer:
V(t) = XLI₀sin(π/2 - ωt)
Explanation:
According to Maxwell's equation which is expressed as;
V(t) = dФ/dt ........(1)
Magnetic flux Ф can also be expressed as;
Ф = LI(t)
Where
L = inductance of the inductor
I = current in Ampere
We can therefore Express Maxwell equation as:
V(t) = dLI(t)/dt ....... (2)
Since the inductance is constant then voltage remains
V(t) = LdI(t)/dt
In an AC circuit, the current is time varying and it is given in the form of
I(t) = I₀sin(ωt)
Substitutes the current I(t) into equation (2)
Then the voltage across inductor will be expressed as
V(t) = Ld(I₀sin(ωt))/dt
V(t) = LI₀ωcos(ωt)
Where cos(ωt) = sin(π/2 - ωt)
Then
V(t) = ωLI₀sin(π/2 - ωt) .....(3)
Because the voltage and current are out of phase with the phase difference of π/2 or 90°
The inductive reactance XL = ωL
Substitute ωL for XL in equation (3)
Therefore, the voltage across inductor is can be expressed as;
V(t) = XLI₀sin(π/2 - ωt)