AeroDynamics: Forces on an Airplane

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Questions and Answers

What is the primary function of a propeller on an aircraft?

  • Generate lift
  • Provide thrust (correct)
  • Create drag
  • Stabilize the aircraft

What does the angle of attack refer to?

  • The angle between fuselage axis and wing chord length
  • The asymmetry between the top and bottom curves of an airfoil
  • The angle between one of the wings and horizontal plane
  • The angle the wind makes with the wing (correct)

Which term refers to the shape of an airfoil that conforms to the streamlines of the flow?

  • Dihedral Angle
  • Camber line (correct)
  • Angle of Attack
  • Angle of Incidence

Which type of aircraft is likely to have a high camber airfoil?

<p>Slow-flying high-lift aircraft (D)</p> Signup and view all the answers

What is the term for the angle between one of the wings and the horizontal plane?

<p>Dihedral Angle (C)</p> Signup and view all the answers

In terms of aerodynamics, what does a high camber airfoil help achieve?

<p>Increased lift (C)</p> Signup and view all the answers

Which term represents the angle between fuselage axis and wing chord length?

<p>Angle of Incidence (B)</p> Signup and view all the answers

What is a propeller's role in relation to an aircraft's motion?

<p>Convert rotational motion into thrust for propulsion (B)</p> Signup and view all the answers

What effect does a high angle of attack have on an aircraft's performance?

<p>Increased lift and drag (D)</p> Signup and view all the answers

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Study Notes

What is Aerodynamics?

  • Deals with the motion and forces acting on a body moving in air
  • Concerned with the study of the interaction between air and solid objects

How Do Airplanes Fly?

  • 4 aerodynamic forces act on an airplane in flight: thrust, drag, lift, and weight
  • Conditions for flight: thrust > drag, lift > weight
  • In straight and level flight, lift and weight are balanced
  • During descent, gravity exceeds lift, and drag must overcome thrust

Forces Acting on a Plane

  • Weight: weight of the airplane acts downwards due to gravity, should be minimized
  • Thrust: mechanical force generated by the engine to move the aircraft forward
  • Lift: mechanical force generated by a solid object moving through a fluid, acts perpendicular to the direction of fluid flow
  • Drag: resisting force to the motion of the aircraft due to its relative motion with air flow

Formulas

  • Lift formula: L = 1/2 ρ A V²C_L
  • Drag formula: D = ρV²C_D/2
  • Bernoulli's equation: (P/ ρg) + (V²/2g) + Z = const

Motion of an Airplane

  • Pitch motion: up and down movement of the nose
  • Rolling motion: rotation around the longitudinal axis
  • Yaw motion: rotation around the vertical axis

Basic Parts of an Airplane

  • Fuselage: main body of the airplane, houses the flight crew, passengers, and cargo
  • Wings: generate lift due to the difference in curvature of the upper and lower parts
  • Tail: provides stability and control to the vertical up-down movement of the nose
  • Stabilizers: keep the aircraft in straight-and-level flight
  • Elevators: control the climb or descent of the aircraft
  • Rudder: defines horizontal flight and provides directional control
  • Ailerons: control the rolling (or banking) motion of the aircraft
  • Flaps: increase lift during takeoff and landing
  • Propeller: provides thrust to the aircraft
  • Airfoil: shape that conforms to the streamlines of the flow and prevents wake formation

Wing Generation of Lift

  • Lift is generated by the difference in pressure above and below the wing
  • Airfoil shape produces better lift than any other form of the wing
  • Camber line: line joining the leading and trailing edges of an airfoil equidistant from the upper and lower surfaces
  • Camber: asymmetry between the top and the bottom curves of an aerofoil in cross-section
  • Angle of incidence: angle between the fuselage axis and the wing chord length
  • Angle of attack: angle the wind makes with the wing (relative wind)
  • Dihedral angle: angle between one of the wings and the horizontal plane in which the fuselage axis is situated

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