__Takeoff Velocity Calculator:__

__Takeoff Velocity Calculator:__

Enter the values of Mass of the Aircraft m_{(kg)}, Accelaration of Gravity g_{(m/s}^{2}_{)}, Coefficient of Lift CL, Surface Area A_{(m}^{2}_{)}, Density of the Air d_{(kg/m}^{3}_{)} to determine the value of Takeoff Velocity V_{(m/s)} .

__Takeoff Velocity Formula:__

__Takeoff Velocity Formula:__

The Takeoff Velocity V_{(m/s)} in meter per second is equal to the SQRT of the Value of 2 into multiply the Mass of the Aircraft m_{(kg)} in kilogram and Accelaration of gravity g_{(m/s}^{2}_{)} in meter per second square and is Divided by the Coefficient of lift CL is multiply to the Surface Area A_{(m}^{2}_{)} in meter square and Density of the air d_{(kg/m}^{3}_{)} in kilogram per meter cube.

The Equation of Takeoff Velocity can be writtern as,

V_{(m/s)} = SQRT ( 2 * m_{(kg)} * g_{(m/s}^{2}_{) }/ ( CL * A_{(m}^{2}_{)} * d_{(kg/m}^{3}_{)} ) )

Here,

V_{(m/s)} = Takeoff Velocity in meter per second

m_{(kg)} = Mass of the Aircraft in kilogram

g_{(m/s}^{2}_{)} = Accelaration of gravity in meter per second square

CL = Coefficient of lift

A_{(m}^{2}_{)} = Surface Area in meter square

d_{(kg/m}^{3}_{)} = Density of the air in kilogram per meter cube

__Takeoff Velocity Calculation :__

__Takeoff Velocity Calculation :__

1)Calculate the Takeoff Velocity and given for Mass of the Aircraft = 3500kg , Coefficient of lift

= .80 , Surface Area = 80m^{2} , Density of the air = 1.220kg/m^{3}.

Answer

V = √( 2 * m * g / ( CL * A * d ))

V = √ ( 2 * 3500 * 9.81 / ( .80 * 80 * 1.220 ) )

V = 29.65m/s.

2)Calculate the Surface Area and given for Mass of the Aircraft = 3500kg , Coefficient of lift

= .80 , Density of the air = 1.220kg/m^{3} , Takeoff Velocity = 29.65m/s.

Answer

V = √( 2 * m * g / ( CL * A * d ))

29.65 = √ ( 2 * 3500 * 9.81 / ( .80 * A * 1.220 ) )

A = 80m^{2}.

__Acceleration of aircraft carrier take-off | One-dimensional motion | Physics |__

__Acceleration of aircraft carrier take-off | One-dimensional motion | Physics |__