Answer:Climatic processes affect the dynamics of Earth's ice sheets and glaciers, and along ... by abrupt events and by continuous reshaping of Earth's surface from surface ... Forecasting natural disasters, including the timing and size of earthquakes, the . Last, human activity has a profound impact on water resources, landscape
Explanation:
step by step
. Methylated spirits have ethanol as a base but may include methyl alcohol (methanol) as part of the denaturing process.
Answer:
A., B., and C.
Explanation:
An Ohmic material is a material that obeys Ohm's Law, V = IR.
In contrast, a non-Ohmic material is one that does not obey Ohm's law.
Ohm's law states that the voltage across an electrical object is proportional to the current flowing through it, with the constant of proportionality being Resistance, R (in Ohm's).
The only Non-Ohmic material is the semiconductor, as semiconductors do not obey Ohm's law.
(a) 0.448
The gravitational potential energy of a satellite in orbit is given by:
![U=-\frac{GMm}{r}](https://tex.z-dn.net/?f=U%3D-%5Cfrac%7BGMm%7D%7Br%7D)
where
G is the gravitational constant
M is the Earth's mass
m is the satellite's mass
r is the distance of the satellite from the Earth's centre, which is sum of the Earth's radius (R) and the altitude of the satellite (h):
r = R + h
We can therefore write the ratio between the potentially energy of satellite B to that of satellite A as
![\frac{U_B}{U_A}=\frac{-\frac{GMm}{R+h_B}}{-\frac{GMm}{R+h_A}}=\frac{R+h_A}{R+h_B}](https://tex.z-dn.net/?f=%5Cfrac%7BU_B%7D%7BU_A%7D%3D%5Cfrac%7B-%5Cfrac%7BGMm%7D%7BR%2Bh_B%7D%7D%7B-%5Cfrac%7BGMm%7D%7BR%2Bh_A%7D%7D%3D%5Cfrac%7BR%2Bh_A%7D%7BR%2Bh_B%7D)
and so, substituting:
![R=6370 km\\h_A = 5970 km\\h_B = 21200 km](https://tex.z-dn.net/?f=R%3D6370%20km%5C%5Ch_A%20%3D%205970%20km%5C%5Ch_B%20%3D%2021200%20km)
We find
![\frac{U_B}{U_A}=\frac{6370 km+5970 km}{6370 km+21200 km}=0.448](https://tex.z-dn.net/?f=%5Cfrac%7BU_B%7D%7BU_A%7D%3D%5Cfrac%7B6370%20km%2B5970%20km%7D%7B6370%20km%2B21200%20km%7D%3D0.448)
(b) 0.448
The kinetic energy of a satellite in orbit around the Earth is given by
![K=\frac{1}{2}\frac{GMm}{r}](https://tex.z-dn.net/?f=K%3D%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7BGMm%7D%7Br%7D)
So, the ratio between the two kinetic energies is
![\frac{K_B}{K_A}=\frac{\frac{1}{2}\frac{GMm}{R+h_B}}{\frac{1}{2}\frac{GMm}{R+h_A}}=\frac{R+h_A}{R+h_B}](https://tex.z-dn.net/?f=%5Cfrac%7BK_B%7D%7BK_A%7D%3D%5Cfrac%7B%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7BGMm%7D%7BR%2Bh_B%7D%7D%7B%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7BGMm%7D%7BR%2Bh_A%7D%7D%3D%5Cfrac%7BR%2Bh_A%7D%7BR%2Bh_B%7D)
Which is exactly identical to the ratio of the potential energies. Therefore, this ratio is also equal to 0.448.
(c) B
The total energy of a satellite is given by the sum of the potential energy and the kinetic energy:
![E=U+K=-\frac{GMm}{R+h}+\frac{1}{2}\frac{GMm}{R+h}=-\frac{1}{2}\frac{GMm}{R+h}](https://tex.z-dn.net/?f=E%3DU%2BK%3D-%5Cfrac%7BGMm%7D%7BR%2Bh%7D%2B%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7BGMm%7D%7BR%2Bh%7D%3D-%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7BGMm%7D%7BR%2Bh%7D)
For satellite A, we have
![E_A=-\frac{1}{2}\frac{GMm}{R+h_A}=-\frac{1}{2}\frac{(6.67\cdot 10^{-11})(5.98\cdot 10^{24}kg)(28.8 kg)}{6.37\cdot 10^6 m+5.97\cdot 10^6 m}=-4.65\cdot 10^8 J](https://tex.z-dn.net/?f=E_A%3D-%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7BGMm%7D%7BR%2Bh_A%7D%3D-%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7B%286.67%5Ccdot%2010%5E%7B-11%7D%29%285.98%5Ccdot%2010%5E%7B24%7Dkg%29%2828.8%20kg%29%7D%7B6.37%5Ccdot%2010%5E6%20m%2B5.97%5Ccdot%2010%5E6%20m%7D%3D-4.65%5Ccdot%2010%5E8%20J)
For satellite B, we have
![E_B=-\frac{1}{2}\frac{GMm}{R+h_B}=-\frac{1}{2}\frac{(6.67\cdot 10^{-11})(5.98\cdot 10^{24}kg)(28.8 kg)}{6.37\cdot 10^6 m+21.2\cdot 10^6 m}=-2.08\cdot 10^8 J](https://tex.z-dn.net/?f=E_B%3D-%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7BGMm%7D%7BR%2Bh_B%7D%3D-%5Cfrac%7B1%7D%7B2%7D%5Cfrac%7B%286.67%5Ccdot%2010%5E%7B-11%7D%29%285.98%5Ccdot%2010%5E%7B24%7Dkg%29%2828.8%20kg%29%7D%7B6.37%5Ccdot%2010%5E6%20m%2B21.2%5Ccdot%2010%5E6%20m%7D%3D-2.08%5Ccdot%2010%5E8%20J)
So, satellite B has the greater total energy (since the energy is negative).
(d) ![-2.57\cdot 10^8 J](https://tex.z-dn.net/?f=-2.57%5Ccdot%2010%5E8%20J)
The difference between the energy of the two satellites is:
![E_B-E_A=-2.08\cdot 10^8 J-(-4.65\cdot 10^8 J)=-2.57\cdot 10^8 J](https://tex.z-dn.net/?f=E_B-E_A%3D-2.08%5Ccdot%2010%5E8%20J-%28-4.65%5Ccdot%2010%5E8%20J%29%3D-2.57%5Ccdot%2010%5E8%20J)
Constant acceleration of plane = 3m/s²
a) Speed of the plane after 4s
Acceleration = speed/time
3m/s² = speed/4s
S = 12m/s
The speed of the plane after 4s is 12m/s.
b) Flight point will be termed as the point the plane got initial speed, u, 20m/s
Find speed after 8s, v
a = 3m/s²
from,
a = <u>v</u><u> </u><u>-</u><u> </u><u>u</u>
t
3 = <u>v</u><u> </u><u>-</u><u> </u><u>2</u><u>0</u>
8
24 = v - 20
v = 44m/s
After 8s the plane would've 44m/s speed.