Home Page |
What is a
Drone? |
History |
Physics |
Applications |
Current
Issues |
References |
L
= ½ ρ v2
A CL
L = Lift
ρ
= Density of Air
v
= Velocity
A
= Surface area
CL
= Coefficient of
Lift
Force of
Gravity
Equation:
FGravity
= m g
m
= mass
g
= gravity (9.8 m/s2)
Thrust
Equations:
FThurst
= A ΔP
FThurst
= ½
A ρ
( Vf2
- Vi2
)
ΔP
= Change
in
Pressure
A = area of
propeller
disks
ρ
= Density of
air ≈
1.2 kg/m3
Vf
= Final
Velocity
Vi2
= Initial
Velocity
D =
½ ρ v2 A CD
D =
Drag
ρ = Density of Air ≈ 1.2 kg/m3
v
= Velocity
A
= Surface area
CD = Coefficient of drag
Voltage Equations:
V
= I R
or
V = P / I
V
= Voltage
P = Power
I = Current