Answer:
The pressure that the container will start to leak is 154.87 psi
Explanation:
Force on end plates F = p(πR²) ⇒ pπR²
There is an equal reaction from four bolts ∴ F = pπR² / 4 .............. (1)
due to force on bolt, each bolt stretch by 
Therefore;
.........................(2)
Leaking will start when tightening is outstretched by half turn per 16 turns per inch.
Cylinder experience a radial expansion as p increases. it is accompanied by poisson contraction
in axial direction. That is, the bolt do not have to experience a long stretch before the pressure breaks off the plate.
...................... (3)
Axial deformation
of cylinder = L times axial ∈₀
<em>see continuation in attached picture in writing to get the value of Pressure: since we have the value of P</em>
R=8", L=16", t=0.125"
Area of bolts 


V for brass = 0.3
![P = \frac{1}{8*8*16} [\frac{0.150*12.5*200*0.125*10^9}{\pi*8*125*0.125+4*0.3*0.150*200}]](https://tex.z-dn.net/?f=P%20%3D%20%5Cfrac%7B1%7D%7B8%2A8%2A16%7D%20%5B%5Cfrac%7B0.150%2A12.5%2A200%2A0.125%2A10%5E9%7D%7B%5Cpi%2A8%2A125%2A0.125%2B4%2A0.3%2A0.150%2A200%7D%5D)
p = 1.67797.183 P ⇒ 154.87 psi
Answer:
C can i have brainliest pleaseee
Explanation:
Explanation:
Compression ratio:
Compression ratio is the ratio of volume .Generally it is denoted by r.From the diagram we can say that the compression ratio r

Generally compression ratio varies from 10 to 14 in petrol engine but on the other hand the compression ratio in diesel engine is more as compare to petrol .In diesel engine the compression ratio varies from 15 to 20.
Yes there is limit of compression ratio in Otto cycle.If compression ratio is high in Otto cycle then there will be more possibility of pre ignition of air fuel and this is called miss firing.This is not good for Otto cycle.
Answer:
The value of exit temperature from the nozzle = 719.02 K
Explanation:
Temperature at inlet
= 450°c = 723 K
Velocity at inlet
= 55 
velocity at outlet
= 390 
Specific heat at constant pressure for steam 
Apply steady flow energy equation for the nozzle


Put all the values in the above formula we get,
⇒ 18723 × 723 +
=
+ 
⇒
= 719.02 K
This is the value of exit temperature from the nozzle.