Complete question:
The exit nozzle in a jet engine receives air at 1200 K, 150 kPa with negligible kinetic energy. The exit pressure is 80 kPa, and the process is reversible and adiabatic. Use constant specific heat at 300 K to find the exit velocity.
Answer:
The exit velocity is 629.41 m/s
Explanation:
Given;
initial temperature, T₁ = 1200K
initial pressure, P₁ = 150 kPa
final pressure, P₂ = 80 kPa
specific heat at 300 K, Cp = 1004 J/kgK
k = 1.4
Calculate final temperature;

k = 1.4

Work done is given as;

inlet velocity is negligible;

Therefore, the exit velocity is 629.41 m/s
Answer:

Explanation:
By energy conservation and work energy theorem we can say that after bullet hits the block, it will move on the rough floor and comes to rest
so here work done by frictional force = change in kinetic energy
so we know that





now by momentum conservation we have



I believe you meant valence electrons?
Sulfur has 6 valence e-, and Silicon has 4.
Hope this helps! :)
<span>1.0x10^3 newtons of force
1.0x10^2 kilograms of weight (assuming local gravity of 9.8 m/s^2)
I will assume that the external pressure is 1 atmosphere (101325 Pascals) since it wasn't specified in the problem. So let's simply multiply the area of the suction cup by the pressure and see what we get:
101325 P * 0.01 m^2
= 101325 kg/(m*s^2) * 0.01 m^2
= 1013.25 kg*m/s^2
= 1013.25 N
So the suction cup can support 1013.25 Newtons of force. Assuming the local gravitational acceleration is 9.8 m/s^2, let's see how many kilograms that is
1013.25 N / 9.8 m/s^2
= 1013.25 kg*m/s^2 / 9.8 m/s^2
= 103.3928571 kg
Rounding to 2 significant figures gives 1.0x10^3 newtons, or 1.0x10^2 kilograms.</span>