Northstar VFR
MAY 26, 2025
When deployed, they increase the wings lift and drag, allowing the airplane to fly safely at slower speeds. When flaps extend, they increase the camber (curvature) of the wing, which boosts the amount of lift the wing generates. On takeoff , flaps help the airplane become airborne sooner by increasing lift.
Pilot Institute
MARCH 13, 2025
Many explanations on websites, videos, and even some textbooks oversimplify or misrepresent the true mechanics of lift. In reality, lift generation involves both Bernoullis principle and Newtons third law working together. Read on to understand Bernoullis principle and how it relates to lift the right way.
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Pilot Institute
FEBRUARY 9, 2025
Wing Control: Flaps, slats, and ailerons change the chord line, impacting lift and control. The Difference Between a Chord Line and a Camber Line The chord line is a straight line that crosses the leading and trailing edges of the airfoil. The mean camber line is drawn halfway between the upper and lower surfaces.
Pilot Institute
JUNE 4, 2025
A tailless airplane is one where everything needed to fly, like lift, control, and stability, is built into the main wing. In level flight, the aircraft is adjusted so that the wingtips dont add lift. Upward Deflection : Raising both elevons decreases the camber of the wing. Lift is reduced, and the nose pitches downward.
Flight Training Central
JANUARY 6, 2025
Frost will change the camber of the wing, increasing its lifting capability. Frost will disrupt the smooth flow of air over the wing, adversely affecting its lifting capability. How will frost on the wings of an airplane affect takeoff performance?
Pilot Institute
FEBRUARY 9, 2025
Wing Control: Flaps, slats, and ailerons change the chord line, impacting lift and control. The Difference Between a Chord Line and a Camber Line The chord line is a straight line that crosses the leading and trailing edges of the airfoil. The mean camber line is drawn halfway between the upper and lower surfaces.
Pilot Institute
SEPTEMBER 30, 2024
The lift and drag imbalance between the left and right ailerons creates adverse yaw. Adverse yaw is an undesirable side effect of lift production, resulting in an uncoordinated, slipping turn. This creates more lift and drag on the upgoing wing (left) and less on the downgoing (right) wing. What is Adverse Yaw?
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