Answer:
I. H = U² Sin²θ/2g
II. R = U² Sin 2θ/g
III. T = 2U Sinθ/g
Step-by-step explanation:
We have a projectile motion with:
U = launch speed of projectile
θ = Angle of launch speed with horizontal surface
Ux = U Sinθ = Horizontal Component of Launch Speed
Uy = U Sinθ = Vertical Component of Launch Speed
H = Maximum Height attained by Projectile
R = Range of Projectile
t = Time to reach maximum height
T = 2t = Total Time of flight
I.
For H:
Considering the vertical motion of projectile, we use 3rd eqn. of motion:
2gh = Vf² - Vi²
here,
Vf = 0 m/s (Because projectile stops at highest point)
Vi = Uy = U Sinθ
g = -g (For upward motion)
h = H
Therefore,
-2gH = 0² - (U Sinθ)²
H = U² Sin²θ/2g
III.
For T:
Considering the vertical motion of projectile, we use 1st eqn. of motion:
Vf = Vi + gt
here,
Vf = 0 m/s (Because projectile stops at highest point)
Vi = Uy = U Sinθ
g = -g (For upward motion)
Therefore,
0 = U Sinθ - gt
t = U Sinθ/g
Therefore,
T = 2t
T = 2U Sinθ/g
II.
For R:
We neglect air resistance in our analysis, sue to which the horizontal velocity of projectile remains constant. Therefore:
S =Vt
where,
S = R
V = Ux = U Cosθ
t = T = 2U Sinθ/g
Therefore,
R = (U Cosθ)(2U Sinθ/g)
R = U²(2 SinθCosθ)/g
Since, Sin 2θ = 2 SinθCosθ
Therefore,
R = U² Sin 2θ/g