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alukav5142 [94]
2 years ago
8

Tin atoms are introduced into a FCC copper crystal, producing an alloy with a lattice pa- rameter of 3.7589 x 10-8 cm and a dens

ity of 8.772 g/cm3. Calculate the atomic percentage of tin present in the alloy.
Engineering
1 answer:
stira [4]2 years ago
7 0

Given:

Lattice parameter, a = 3.7589\times 10^{-8}cm

density, \rho = 8.772g/cm^{3}\\

Solution:

We know that  for FCC, total no. of atoms in a crystal lattice = 4

let the number of atoms in Tin for alloying be 'n'

⇒ Total no. of Copper atoms in the alloy,  = 4 - n

Also mass of Copper, m = 63.54 g/mol

atomic mass of Tin = 118.69 g/mol

We Know density of the crystal lattice is given by the formula:

\rho = \frac{m\times Z}{a^{3}\times N_{A}}                 (1)

where,

N_{A} = Avagadro's number =  6.23\times 10_{23}

Putting all the values in eqn (1), we get

8.772 = \frac{118.69\times x\times (4 - n)\times 63.54}{(3.7589\times 10^{-8})^{3}\times 6.023\times 10^{23}}

280.6 = 55.15n +254.16

n = 0.479 atoms/cell

Now to calculate the atomic percentage of Tin present in the alloy:

atomic percentage = \frac{no. of atoms in Tin/cell}{Total no. of atoms in FCC lattice}

atomic % Tin present in alloy = \frac{0.479}{4} = 0.1198\times 100

atomic % Tin present in alloy = 11.98%

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Leto [7]

Answer:

The rate of heat transfer from both sides of the plate to the air is 240 W

Explanation:

Given;

area of the flat plate = 0.2 m × 0.2 m = 0.04 m²

velocity of atmospheric air stream, v = 40 m/s

drag force, F =  0.075 N

The rate of heat transfer from both sides of the plate to the air:

q = 2 [h'(A)(Ts -T∞)]

where;

h' is heat transfer coefficient obtained from Chilton-Colburn analogy

h' = \frac{C_f}{2} \rho u C_p P_r^{-2/3}\\\\\frac{C_f}{2} = \frac{\tau'_s}{2*\rho u^2/2}

Properties of air at 70°C and 1 atm:

ρ = 1.018 kg/m³, cp = 1009 J/kg.K, Pr = 0.7, v = 20.22 x 10⁻⁶ m²/s

\frac{C_f}{2} = \frac{(0.075/2)/(0.2)^2}{2*(1.018)(40)^2/2} = 5.756*10^{-4}\\\\Thus,\\h' = 5.756*10^{-4} (1.018*40*1009)*(0.7)^{-2/3}\\\\h' = 30 \ W/m^2.K

Finally;

q = 2 [ 30(0.04)(120 - 20) ]

q = 240 W

Therefore, the rate of heat transfer from both sides of the plate to the air is 240 W

4 0
2 years ago
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The rate of flow through an ideal clarifier is 8000m3 /d, the detention time is 1h and the depth is 3m. If a full-length movable
Fittoniya [83]

Answer:

a) 35%

b) yes it can be improved by moving the tray near the top

   Tray should be located ( 1 to 2 meters below surface )

   max removal efficiency ≈ 70%

c) The maximum removal will drop as the particle settling velocity = 0.5 m/h

Explanation:

Given data:

flow rate = 8000 m^3/d

Detention time = 1h

depth = 3m

Full length movable horizontal tray :  1m below surface

<u>a) Determine percent removal of particles having a settling velocity of 1m/h</u>

velocity of critical sized particle to be removed = Depth / Detention time

= 3 / 1 = 3m/h

The percent removal of particles having a settling velocity of 1m/h ≈ 35%

<u>b) Determine if  the removal efficiency of the clarifier can be improved by moving the tray, the location of the tray  and the maximum removal efficiency</u>

The tray should be located near the top of the tray ( i.e. 1 to 2 meters below surface ) because here the removal efficiency above the tray will be 100% but since the tank is quite small hence the

Total Maximum removal efficiency

=  percent removal_{above} + percent removal_{below}

= ( d_{a},v_{p} ) . \frac{d_{a} }{depth}  + ( d_{a},v_{p} ) . \frac{depth - d_{a} }{depth}  = 100

hence max removal efficiency ≈ 70%

<u>c) what is the effect of moving the tray would be if the particle settling velocity were equal to 0.5m/h?</u>

The maximum removal will drop as the particle settling velocity = 0.5 m/h

7 0
2 years ago
If the current on your power supply exceeds 500 mA it can damage the supply. Suppose the supply is set for 37 V. What is the sma
lilavasa [31]

Answer:

74 Ω

Explanation:

Data provided in the question:

Maximum value of the current that can be provided = 500 mA

= 500 × 10⁻³ A  

Applied voltage set for the system = 37 V

Now,  

The smallest resistance that can be measured    

= [ Applied voltage ] ÷ [ Maximum current that can be applied ]

= 37 ÷ (  500 × 10⁻³ )

= 74 Ω

4 0
2 years ago
The fatigue data for a brass alloy are given as follows: Stress Amplitude (MPa) Cycles to Failure 170 3.7 × 104 148 1.0 × 105 13
prohojiy [21]

Answer:

i) S–N plot is attached

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Explanation:

i) I have attached the S–N plot (stress amplitude versus logarithm of cycles to failure)

ii) The question says we should find the fatigue strength at 4 × 10^(6) cycles.

So let's find the log of this and trace it on the graph attached.

Log(4 × 10^(6)) = 6.6

From the graph attached, at log of cycle value of 6.6, the fatigue strength is approximately 100 MPa

iii) The question says we should find the fatigue life for 120 MPa.

Thus, from the graph, at stress amplitude of 120 MPa, the log of cycles is approximately 5.75.

Thus,the fatigue life will be the inverse log of 5.75.

Thus, fatigue life = 10^(5.75)

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8 0
2 years ago
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sp2606 [1]

Answer: 0.021818m =2.18x10^-²m

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T = Wall thickness

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Radius= diameter/2 =4/2=2m

Design stress=Hoop stress =Pr/t where p=internal pressure or internal pressure, r=radius and t= wall thickness.

As Laplace equation stated.

110,000,000= 1,2000,00 x 2/t

t= 2,400,000/110,000,000.

t= 0.021818m

t=2.18x10^-2m.

3 0
2 years ago
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