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Keith_Richards [23]
3 years ago
6

If the velocity of gas molecules is doubled, then it’s kinetic energy will?( hint formula for kinetic energy is KE=.5 x mv2)

Physics
2 answers:
eduard3 years ago
7 0

Answer:

D quadruple

Explanation:

E = \frac{1}{2}mv^2\\E'=\frac{1}{2}m(2v)^2=\frac{1}{2}m4 v^2 = 4(\frac{1}{2}mv^2)=4E

AysviL [449]3 years ago
3 0

Answer:

(D) quadruple

Explanation:

KE_{1} = \frac{1}{2}m v^{2} -----equation 1

where;

KE₁ is the initial kinetic energy

m is the gas molecule mass

v is the velocity of gas molecules

⇒ When the velocity of gas molecules is doubled (2v)

KE_{2} = \frac{1}{2}m (2v)^{2}

KE_{2} = \frac{1}{2}m*4v^{2}

KE_{2} = 4(\frac{1}{2}mv^2) -------equation 2

Recall; From equation 1;

KE_{1} = \frac{1}{2}m v^{2}

Substitute in KE₁ in equation 2

KE₂ = 4(KE₁)

Therefore, the kinetic energy will quadruple

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the idling engines of a landing turbojet produce forward thrust when operating in a normal manner, but they can produce reverse
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Forward thrust has positive values and reverse thrust has negative values.

Thrust is a sudden push or pull in a certain direction.

a)

Flight speed u = 150 km/h

1 km/h = \frac{1}{3.6} km/s

therefore, 150 km/h =  41.67 km / s

The thrust force represents the horizontal or x-component of momentum equation:

T = m_{exhaust} * U_{exhaust} - U_{flight}

T = 50 * (150 - 41.67)

T = 5416.67 N

Therefore, the value of forward thrust is 5416.67 N.

b)

Now the exhaust velocity is now vertical due to reverse thrust application, then it has a zero horizontal component,

thus thrust equation is:

T = m_{exhaust} * U_{exhaust} - U_{flight}

T = 50 * (0 - 41.67)

T = -2083.5 N

Therefore, the thrust force T is -2083.5 N in the reverse direction.

c)

Now the exhaust velocity and flight velocity is zero, then it has a zero horizontal component, thus thrust is also zero becauseU_{exhaust} = U_{flight} = 0\\

T = 0

Therefore, there is no difference in two velocities in x direction.

The given question is incomplete, the complete question is,

"The idling engines of a landing turbojet produce forward thrust when operating in a normal manner, but they can produce reverse thrust if the jet is properly deflected. Suppose that while the aircraft rolls down the runway at 150 km/h the idling engine consumes air at 50 kg/s and produces an exhaust velocity of 150 m/s.

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c. What are the magnitude and direction of the thrust (forward or reverse) after the plane has come to a stop, with 90 degree exhaust deflection and an airflow of 40 kg/s?"

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1 year ago
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