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.
Lift, thrust, drag, and gravity affects all flying objects and wildlife. The blades of the helicopter provide lift, drag and thrust.
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 production of lift creates induced drag. To create more lift, more airspeed is needed, and with airspeed, comes drag.
LIFT -- force provided by the wing and in perpendicular direction to the wing. In straight and level flight the lift is exactly equal to the aircraft weight. WEIGHT -- the force pulling vertically down on the airplane due to gravity. In straight and level flight this is equal to the lift. THRUST -- the force that pulls the airplane forward, provided by the propeller or jet engine. If the airplane is flying at a constant speed in level flight, this thrust is exactly equal to the drag. DRAG -- the aerodynamic force on the airplane in the opposite direction of its travel. Drag is due to skin friction, form drag (drag around wheels, struts, etc) and induced drag (produced by the wing as a side effect of lift)
Drag
A higher angle of attack has an increase of both lift and drag.
Lift, thrust, drag, and gravity affects all flying objects and wildlife. The blades of the helicopter provide lift, drag and thrust.
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 production of lift creates induced drag. To create more lift, more airspeed is needed, and with airspeed, comes drag.
coefficient of drag in 0 lift
lift decrease and increase drag
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 .
For no lift, The induced drag will be zero. However, there will still be drag due to viscous forces and pressure forces.
LIFT -- force provided by the wing and in perpendicular direction to the wing. In straight and level flight the lift is exactly equal to the aircraft weight. WEIGHT -- the force pulling vertically down on the airplane due to gravity. In straight and level flight this is equal to the lift. THRUST -- the force that pulls the airplane forward, provided by the propeller or jet engine. If the airplane is flying at a constant speed in level flight, this thrust is exactly equal to the drag. DRAG -- the aerodynamic force on the airplane in the opposite direction of its travel. Drag is due to skin friction, form drag (drag around wheels, struts, etc) and induced drag (produced by the wing as a side effect of lift)
drag you pull across the ground lift you pick up and take around
Lift, weight, thrust and drag.
Lift is equal to drag, so if the drag was 12000N (newtons) the lift would be 12000N. it is mainly used for slowing the aircraft down for decend.