When thrust and drag are equal, the plane's speed remains constant. The forces are balanced, and the plane will maintain its current velocity without accelerating or decelerating. This state is known as "steady level flight."
When the thrust force is equal to the drag force, the object will maintain a constant velocity (assuming no other forces are acting on it). This state is known as dynamic equilibrium, where the forces are balanced and there is no acceleration.
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)
The main forces acting on a plane in flight are lift, weight, thrust, and drag. Lift is produced by the wings, opposing the weight of the plane. Thrust is provided by the engines, moving the plane forward and countering drag, which is the aerodynamic force slowing the plane down.
The forces acting on a plane flying at a constant height include lift, weight, thrust, and drag. Lift counters weight to keep the plane in the air, and thrust is provided by the engines to overcome drag and maintain speed.
A plane uses thrust, generated by its engines, to propel itself forward in the air. This thrust overcomes drag to propel the plane forward and generate lift, allowing the plane to stay airborne.
The car (or plane/whatever else it is) accelerates. This means that it gains speed
When the thrust force is equal to the drag force, the object will maintain a constant velocity (assuming no other forces are acting on it). This state is known as dynamic equilibrium, where the forces are balanced and there is no acceleration.
If the thrust of a plane becomes greater than the drag, the aircraft will accelerate forward. This increase in speed can lead to the plane climbing if the lift generated by the wings also exceeds the weight of the aircraft. However, if the thrust continues to significantly exceed drag, the plane will gain altitude and speed until it reaches a new equilibrium or until other factors (like engine limits or air density) come into play.
Lift,Drag,Weight,Thrust.
Weight, lift, drag, thrust.
The main forces acting on a plane in flight are lift, weight, thrust, and drag. Lift is produced by the wings, opposing the weight of the plane. Thrust is provided by the engines, moving the plane forward and countering drag, which is the aerodynamic force slowing the plane down.
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)
By overcoming gravity with lift and drag with thrust.
The forces acting on a plane flying at a constant height include lift, weight, thrust, and drag. Lift counters weight to keep the plane in the air, and thrust is provided by the engines to overcome drag and maintain speed.
Thrust on a plane is the forward force produced by the aircraft's engines, which propels it through the air. It is essential for overcoming drag and achieving lift, allowing the plane to take off, maintain flight, and maneuver. Thrust is generated by jet engines or propellers and is measured in pounds or Newtons. The balance of thrust with drag, lift with weight, is crucial for stable flight.
If thrust is greater than drag on an airplane, the aircraft will accelerate forward. This surplus thrust allows the plane to gain speed, which is essential for takeoff and climbing. As the speed increases, the lift generated by the wings also increases, enabling the aircraft to ascend. In essence, a net positive thrust leads to improved performance and maneuverability.
A plane uses thrust, generated by its engines, to propel itself forward in the air. This thrust overcomes drag to propel the plane forward and generate lift, allowing the plane to stay airborne.