The production of lift creates induced drag. To create more lift, more airspeed is needed, and with airspeed, comes drag.
To overcome drag. The four forces always acting on an airplane in flight are: Lift, thrust, gravity, and drag.
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.
Lift, thrust, drag, and gravity affects all flying objects and wildlife. The blades of the helicopter provide lift, drag and thrust.
Drag
The production of lift creates induced drag. To create more lift, more airspeed is needed, and with airspeed, comes drag.
Have enough lift the overcome weight and enough thrust to overcome drag and you will!
hi--jassi
lift and thrust overcome weight and drag
To overcome drag. The four forces always acting on an airplane in flight are: Lift, thrust, gravity, and drag.
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.
Lift, Drag, Thrust, and Weight. (Not counting Money)
lift decrease and increase drag
coefficient of drag in 0 lift
there are four forces that must equalize essentially.... lift and weight , thrust and drag... thrust is produced by engine through jet or propeller and must equal or overcome drag which is created by friction and the effects of air pressures over the surfaces of the craft lift is produced by the forward motion of the airfoil (wing surfaces) and must equal and/or overcome the force of gravity (weight) thrust and lift work to keep the aircraft in flight, while drag and weight work to bring it down that is a really simplified answer though
Lift, thrust, drag, and gravity affects all flying objects and wildlife. The blades of the helicopter provide lift, drag and thrust.
For no lift, The induced drag will be zero. However, there will still be drag due to viscous forces and pressure forces.