Explanation:
see the attachment.. hope it will help you
Answer:

Explanation:
From the question we are told that:
Mass 
Initial heat of pan 
Final heat of pan
Generally the equation for Heat energy released is mathematically given by


Answer:
it is missing some numbers
Explanation:
Answer:
h≅ 58 m
Explanation:
GIVEN:
mass of rocket M= 62,000 kg
fuel consumption rate = 150 kg/s
velocity of exhaust gases v= 6000 m/s
Now thrust = rate of fuel consumption×velocity of exhaust gases
=6000 × 150 = 900000 N
now to need calculate time t = amount of fuel consumed÷ rate
= 744/150= 4.96 sec
applying newton's law
M×a= thrust - Mg
62000 a=900000- 62000×9.8
acceleration a= 4.71 m/s^2
its height after 744 kg of its total fuel load has been consumed


h= 58.012 m
h≅ 58 m
Answer:
114.075 N
798.525 Nm
Explanation:
C = Drag coefficient = 0.5
ρ = Density of air = 1.2 kg/m³
A = Surface area = 9 m²
v = Velocity of wind = 6.5 m/s
r = Height of the tree = 7 m
Drag equation

Magnitude of the drag force of the wind on the canopy is 114.075 N
Toque is given by the product of force and radius

Torque exerted on the tree, measured about the point where the trunk meets the ground is 798.525 Nm