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Dynamic Lift - Newton's Lift, takes effect when a bird changes its body angle slightly upward to it's flight path Induced Lift - Bernoullian Lift, pressure difference between upper and lower areas of a bird's wing Dynamic - Force in motion Daniel Bernoulli - Discoverer of relationship between pressure and fluids in motion

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Billy Mitchell Aerospace Test
Questions & Answers| A
Guaranteed
Dynamic Lift - ✔✔Newton's Lift, takes effect when a bird changes its body angle slightly upward to
it's flight path



Induced Lift - ✔✔Bernoullian Lift, pressure difference between upper and lower areas of a bird's wing



Dynamic - ✔✔Force in motion



Daniel Bernoulli - ✔✔Discoverer of relationship between pressure and fluids in motion



Bernoulli's Principle - ✔✔When a fluid accelerates, the pressure drops



Newton's 1st Law - ✔✔An object at rest remains at rest unless acted upon by an outside force



Newton's 2nd Law - ✔✔A force acting upon a body causes it to accelerate in the direction of
the force; acceleration is directly proportional to the mass of the body being accelerated

, Newton's 3rd Law - ✔✔For every action, there is an equal and opposite reaction



Trailing Edge - ✔✔The back portion of an airfoil



Coefficient of Lift Formula - ✔✔Mathematical formula with 5 components: air density, velocity,
wing area, airfoil design, angle of attack



Camber - ✔✔Curved part of the airfoil that goes from the leading edge to the trailing edge



Leading Edge - ✔✔The front portion of an airfoil



Relative Wind - ✔✔The flow of air which moves opposite the flight path of an airplane



Natural Forces of Flight - ✔✔Drag and Gravity



Forces of Flight - ✔✔Lift, Thrust, Weight (Gravity), Drag



Thrust - ✔✔Moves an aircraft forward



Drag - ✔✔Force that retards forward movement of the aircraft



Chord - ✔✔Imaginary Line drawn from the leading edge to the trailing edge of an airfoil



Lift - ✔✔Upward force that opposes gravity



Angle of Attack - ✔✔Angle between the chord line and the relative wind



Critical Angle of Attack - ✔✔The point at which a wing will stall

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