Answer:
45.3 MN
Explanation:
The forging force at the end of the stroke is given by
F = Y.π.r².[1 + (2μr/3h)]
The final height, h is given as h = 100/2
h = 50 mm
Next, we find the final radius by applying the volume constancy law
volumes before deformation = volumes after deformation
π * 75² * 2 * 100 = π * r² * 2 * 50
75² * 2 = r²
r² = 11250
r = √11250
r = 106 mm
E = In(100/50)
E = 0.69
From the graph flow, we find that Y = 1000 MPa, and thus, we apply the formula
F = Y.π.r².[1 + (2μr/3h)]
F = 1000 * 3.142 * 0.106² * [1 + (2 * 0.2 * 0.106/ 3 * 0.05)]
F = 35.3 * [1 + 0.2826]
F = 35.3 * 1.2826
F = 45.3 MN
Answer:
Between 35°– 45°
Explanation:
In the vertical position, Point the flame in the direction of travel. Keep the flame tip at the correct height above the base metal. An angle of 35°–45° should be maintained between the torch tip and the base metal. This angle may be varied up or down to heat or cool the weld pool if it is too narrow or too wide
Technician A is correct. Technician B is wrong because a gear's transmission is used to increase or decrease torque.
The relation torque is relying on multiplying the circumferential detail with the resource of the usage of the radius; massive gears experience a greater amount of torque, at the same time as smaller gears experience a great deal much less torque. Similarly, the torque ratio is equal to the ratio of the gears' radii. A gear's transmission torque modifications as it will boom or decreases speed. Commonly, with the resource of the usage of lowering the speed, a small torque on the doorway issue is transferred as a massive torque at the output issue. The calculation of torque is quantified with the resource of the usage of an extensive form of teeth.
Learn more about the torque at brainly.com/question/28220969
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Answer: The exit temperature of the gas in deg C is
.
Explanation:
The given data is as follows.
= 1000 J/kg K, R = 500 J/kg K = 0.5 kJ/kg K (as 1 kJ = 1000 J)
= 100 kPa, ![V_{1} = 15 m^{3}/s](https://tex.z-dn.net/?f=V_%7B1%7D%20%3D%2015%20m%5E%7B3%7D%2Fs)
![T_{1} = 27^{o}C = (27 + 273) K = 300 K](https://tex.z-dn.net/?f=T_%7B1%7D%20%3D%2027%5E%7Bo%7DC%20%3D%20%2827%20%2B%20273%29%20K%20%3D%20300%20K)
We know that for an ideal gas the mass flow rate will be calculated as follows.
![P_{1}V_{1} = mRT_{1}](https://tex.z-dn.net/?f=P_%7B1%7DV_%7B1%7D%20%3D%20mRT_%7B1%7D)
or, m = ![\frac{P_{1}V_{1}}{RT_{1}}](https://tex.z-dn.net/?f=%5Cfrac%7BP_%7B1%7DV_%7B1%7D%7D%7BRT_%7B1%7D%7D)
=
= 10 kg/s
Now, according to the steady flow energy equation:
![mh_{1} + Q = mh_{2} + W](https://tex.z-dn.net/?f=mh_%7B1%7D%20%2B%20Q%20%3D%20mh_%7B2%7D%20%2B%20W)
![h_{1} + \frac{Q}{m} = h_{2} + \frac{W}{m}](https://tex.z-dn.net/?f=h_%7B1%7D%20%2B%20%5Cfrac%7BQ%7D%7Bm%7D%20%3D%20h_%7B2%7D%20%2B%20%5Cfrac%7BW%7D%7Bm%7D)
![C_{p}T_{1} - \frac{80}{10} = C_{p}T_{2} - \frac{130}{10}](https://tex.z-dn.net/?f=C_%7Bp%7DT_%7B1%7D%20-%20%5Cfrac%7B80%7D%7B10%7D%20%3D%20C_%7Bp%7DT_%7B2%7D%20-%20%5Cfrac%7B130%7D%7B10%7D)
![(T_{2} - T_{1})C_{p} = \frac{130 - 80}{10}](https://tex.z-dn.net/?f=%28T_%7B2%7D%20-%20T_%7B1%7D%29C_%7Bp%7D%20%3D%20%5Cfrac%7B130%20-%2080%7D%7B10%7D)
= 5 K
= 5 K + 300 K
= 305 K
= (305 K - 273 K)
= ![32^{o}C](https://tex.z-dn.net/?f=32%5E%7Bo%7DC)
Therefore, we can conclude that the exit temperature of the gas in deg C is
.