Lift force for a helicopter is calculated using the following formula: Lift force = mass x acceleration due to gravity x vertical velocity. In this case, the mass would be 4510 kg, the acceleration due to gravity is 9.8 m/s², and the vertical velocity is the rate at which the helicopter is accelerating upward.
Calculating lift force is important for understanding the performance and capabilities of a helicopter. It helps determine the maximum weight that a helicopter can carry and the amount of power needed for it to take off and maintain its altitude.
The lift force of a helicopter is directly proportional to its mass. This means that as the mass increases, the lift force also increases. So, a helicopter with a heavier mass will require more lift force to stay airborne.
The lift force of a helicopter can be affected by several factors, including the design and shape of the rotor blades, the angle of attack of the blades, air density, and the speed of the helicopter. Changes in any of these factors can result in changes in the lift force of the helicopter.
The lift force of a helicopter is directly related to its acceleration. As the helicopter accelerates upward, the lift force must increase to counteract the increase in weight due to the acceleration. This allows the helicopter to maintain its altitude and continue moving upward.