B Airplanes stay level at higher velocities?

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A normal winged airplane maintains level flight at higher speeds by managing lift and drag through control surfaces like elevators and trim settings. As speed increases, lift generated by the wings also increases, which can cause the aircraft to ascend unless adjustments are made. Pilots can push the yoke forward to lower the elevator flaps, reducing lift and directing thrust downwards to maintain altitude. Additionally, using trim allows for sustained adjustments without continuous yoke input. These aerodynamic controls enable pilots to balance speed and altitude effectively.
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Hi,

I was wondering- how would a normal winged airplane (jet/propeller) stay level as it increased in speed? In other words, increasing the velocity over an airfoil will generate more lift. But what if a pilot just wants to go faster and not higher? Where does that increased upward force from induced drag over a wing because a pilot wants to go faster go? thanks!
 
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Modern aircraft both civil and military have adjustable wing configuration depending on the present situation.
The most obvious examples being flaps on the rear of the wing and slats on their leading edge.
This is good for take off and landing, but they get tucked back into the main wing structure for normal flight as they just create needless drag on the aircraft.
 
They can push the yoke ('steering wheel') forward, which pushes down the elevator flaps on the tail, which in turn pushes the tail up, thereby pointing the plane's nose down a bit. That reduces the lift from the wings as well as directing some of the propulsion of the jets towards pushing the plane downwards.

If they want to sustain this setting they can change the 'trim', which activates little extra flaps on the ends of the elevator flaps. 'Trim down' makes these little flaps go up, which makes the airflow push the elevators down (hence removing the need to use the yoke to do this), which in turn points the plane downwards.
 
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