Gravity Drag Lift Friction
Lift,Drag,Weight,Thrust.
The production of lift creates induced drag. To create more lift, more airspeed is needed, and with airspeed, comes drag.
lift decrease and increase drag
coefficient of drag in 0 lift
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.
A higher angle of attack has an increase of both lift and 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 you pull across the ground lift you pick up and take around
Lift, weight, thrust and drag.
due to the pressure on the aileron which goes down gets more lift and very extra little drag,while on other wing the lift is spoilt and the drag greatky increased. thus we have a large rolling effect in the right direction combined with a yawing effect, also in the right direction... . . . . . this one is the right anser for rolling effect with yawing