it makes the lift increase a lot but is slow the plane down a lot as well that is why the pilots like me use is when we are landing a plane.
The four forces of flight are lift, weight (gravity), thrust, and drag. These forces affect planes by enabling the plane to generate lift to counteract gravity (weight), provide thrust for forward motion, and counteract drag to maintain speed and altitude during flight.
Thrust from the helicopter's rotor blades generates lift, which enables the helicopter to overcome gravity and stay airborne. Drag acts as a resistance opposing the helicopter's forward movement, requiring additional thrust to maintain speed. Gravity affects the helicopter by constantly pulling it downward, necessitating continuous lift to counteract and remain in the air.
It is thrust, lift, drag and weightthat affect an aircraft's ability to fly. It is thrust that moves the aircraft forward through the air. The thrust overcomes drag and provides (with the wings) lift to overcome weight.
The zero lift drag coefficient of a Boeing 747 is approximately 0.022. This value represents the drag force experienced by the aircraft when it is not generating lift.
The flow over an airfoil affects its lift and drag characteristics by creating differences in air pressure above and below the airfoil. This pressure difference generates lift, which is the force that allows an aircraft to stay airborne. The flow also creates drag, which is the resistance that opposes the motion of the aircraft. The shape and angle of the airfoil, as well as the speed and density of the air, all play a role in determining the lift and drag forces acting on the airfoil.
A higher angle of attack has an increase of both lift and drag.
lift decrease and increase drag
coefficient of drag in 0 lift
The four forces of flight are lift, weight (gravity), thrust, and drag. These forces affect planes by enabling the plane to generate lift to counteract gravity (weight), provide thrust for forward motion, and counteract drag to maintain speed and altitude during flight.
Thrust from the helicopter's rotor blades generates lift, which enables the helicopter to overcome gravity and stay airborne. Drag acts as a resistance opposing the helicopter's forward movement, requiring additional thrust to maintain speed. Gravity affects the helicopter by constantly pulling it downward, necessitating continuous lift to counteract and remain in the air.
For no lift, The induced drag will be zero. However, there will still be drag due to viscous forces and pressure forces.
The flight of a body mainly depends on its response to the atmospheric air, the shape of the body & the forces acting on the body i.e lift, drag, thrust & weight. The two forces lift & drag are the ones primly influenced by the shape of the body and account to the aerodynamic nature of the body. Every body produces certain amount of lift & drag but its only the measure of these forces affect the flight. More lift helps the body to sustain flight ; less drag accounts for more aerodynamic nature of the body i.e, less lift/thrust is required to sustain the flight and viceversa .
It is thrust, lift, drag and weightthat affect an aircraft's ability to fly. It is thrust that moves the aircraft forward through the air. The thrust overcomes drag and provides (with the wings) lift to overcome weight.
The zero lift drag coefficient of a Boeing 747 is approximately 0.022. This value represents the drag force experienced by the aircraft when it is not generating lift.
drag you pull across the ground lift you pick up and take around
Lift, weight, thrust and drag.
The flow over an airfoil affects its lift and drag characteristics by creating differences in air pressure above and below the airfoil. This pressure difference generates lift, which is the force that allows an aircraft to stay airborne. The flow also creates drag, which is the resistance that opposes the motion of the aircraft. The shape and angle of the airfoil, as well as the speed and density of the air, all play a role in determining the lift and drag forces acting on the airfoil.