Power System Instrumentation December 23, 2025July 15, 2024 by u930973931_answers 50 min Score: 0 Attempted: 0/50 Subscribe 1. Which law explains the lift generation on an aircraft wing? (A) Newtonâs First Law (B) Bernoulliâs Principle (C) Newtonâs Second Law (D) Hookeâs Law 2. What is the primary function of the horizontal stabilizer? (A) Provide lift (B) Control yaw (C) Control pitch (D) Reduce drag 3. What is the angle between the chord line of an airfoil and the direction of the relative wind called? (A) Angle of incidence (B) Angle of attack (C) Dihedral angle (D) Sweep angle 4. The Mach number is defined as the ratio of an objectâs speed to the speed of what? (A) Light (B) Sound (C) Water (D) Wind 5. Which part of an aircraft generates the most lift? (A) Fuselage (B) Wings (C) Tail (D) Engines 6. What does the term âstallâ refer to in aviation? (A) Engine failure (B) Over-speeding (C) Loss of lift (D) Structural failure 7. What is the purpose of winglets on an aircraft? (A) Reduce drag (B) Increase lift (C) Improve stability (D) Decrease weight 8. In which layer of the atmosphere do commercial jets typically cruise? (A) Troposphere (B) Mesosphere (C) Stratosphere (D) Thermosphere 9. What is the name of the point at which the airflow separates from the surface of an airfoil? (A) Separation point (B) Boundary layer (C) Stagnation point (D) Laminar flow 10. Which control surface is primarily responsible for controlling the roll of an aircraft? (A) Aileron (B) Elevator (C) Rudder (D) Flaps 11. What is the primary function of the rudder on an aircraft? (A) Control roll (B) Control yaw (C) Control pitch (D) Provide lift 12. What is the term for the upward force that counteracts an aircraftâs weight? (A) Thrust (B) Drag (C) Gravity (D) Lift 13. Which type of drag is caused by the friction of air flowing over the surface of an aircraft? (A) Induced drag (B) Wave drag (C) Parasite drag (D) Profile drag 14. What is the main purpose of an aircraftâs flaps? (A) Reduce drag during cruise (B) Control yaw (C) Increase lift during takeoff and landing (D) Increase speed 15. The term âsupersonicâ refers to speeds greater than which multiple of the speed of sound? (A) 0.5 (B) 1.5 (C) 1 (D) 2 16. Which type of engine is most commonly used in commercial jet aircraft? (A) Turbofan engine (B) Turboprop engine (C) Piston engine (D) Ramjet engine 17. What is the purpose of an aircraftâs ailerons? (A) Control pitch (B) Control roll (C) Control yaw (D) Increase lift 18. Which term describes the force that resists the motion of an aircraft through the air? (A) Drag (B) Lift (C) Thrust (D) Weight 19. What is the name of the path an aircraft follows over the ground? (A) Flight path (B) Glide path (C) Airway (D) Track 20. What phenomenon occurs when an aircraft exceeds the speed of sound? (A) Vortex generation (B) Turbulence (C) Shock wave formation (D) Laminar flow 21. Which component of the aircraft provides stability and control during flight? (A) Winglets (B) Fuselage (C) Engine (D) Empennage 22. What is the primary function of the aircraftâs fuselage? (A) House crew, passengers, and cargo (B) Provide thrust (C) Generate lift (D) Control yaw 23. Which instrument indicates an aircraftâs speed relative to the surrounding air? (A) Airspeed indicator (B) Altimeter (C) Vertical speed indicator (D) Heading indicator 24. What is the effect of deploying spoilers on an aircraft wing? (A) Reduce lift (B) Decrease drag (C) Increase lift (D) Increase speed 25. Which part of the aircraft reduces the tendency to yaw? (A) Ailerons (B) Horizontal stabilizer (C) Winglets (D) Vertical stabilizer 26. What is the critical angle of attack? (A) The angle at which lift is maximized (B) The angle at which an aircraft will stall (C) The angle at which drag is minimized (D) The angle at which thrust is maximized 27. Which type of aircraft structure is characterized by a stressed skin design? (A) Semi-monocoque (B) Monocoque (C) Truss (D) Composite 28. What is the main advantage of a swept wing design? (A) Increased lift (B) Enhanced stability (C) Improved low-speed performance (D) Reduced drag at high speeds 29. What does the term âaerodynamic centerâ refer to? (A) The point where lift is concentrated (B) The point where drag is minimized (C) The point where all aerodynamic forces act (D) The point where stability is maximized 30. Which flight control surface is used to change an aircraftâs pitch attitude? (A) Ailerons (B) Elevators (C) Rudder (D) Flaps 31. What is the primary purpose of vortex generators on an aircraft wing? (A) Delay flow separation (B) Reduce drag (C) Increase lift (D) Improve control 32. Which type of wing planform has a constant chord along its entire span? (A) Rectangular wing (B) Elliptical wing (C) Tapered wing (D) Delta wing 33. What is the primary function of the landing gear? (A) Absorb landing impacts (B) Provide lift during takeoff (C) Control aircraft direction (D) Increase speed 34. Which of the following is a primary flight control surface? (A) Flaps (B) Slats (C) Spoilers (D) Rudder 35. What is the term for the distance between the leading edge and the trailing edge of a wing? (A) Chord (B) Span (C) Camber (D) Dihedral 36. What is the primary effect of increasing the camber of an airfoil? (A) Increase drag (B) Decrease lift (C) Increase lift (D) Decrease drag 37. Which component of the aircraft is primarily responsible for controlling pitch and yaw during takeoff? (A) Rudder (B) Elevators (C) Ailerons (D) Flaps 38. What is the purpose of dihedral angle in wing design? (A) Improve roll stability (B) Increase lift (C) Reduce drag (D) Increase speed 39. Which type of propulsion system is commonly used in modern commercial airliners? (A) Turbofan (B) Turbojet (C) Turboprop (D) Ramjet 40. What is the function of the nacelle on an aircraft engine? (A) Reduce drag (B) Protect the engine (C) Increase thrust (D) Improve stability 41. What is the main purpose of a flight data recorder? (A) Record flight parameters (B) Monitor engine performance (C) Record cockpit conversations (D) Track aircraft location 42. Which term describes the lift generated by a wing in the presence of downwash? (A) Differential lift (B) Parasite lift (C) Profile lift (D) Induced lift 43. What is the primary function of the pitot tube on an aircraft? (A) Measure airspeed (B) Measure altitude (C) Measure temperature (D) Measure pressure 44. Which flight control surface is used to change an aircraftâs yaw attitude? (A) Elevators (B) Rudder (C) Ailerons (D) Flaps 45. What is the term for the imaginary line from the leading edge to the trailing edge of an airfoil? (A) Camber line (B) Mean aerodynamic chord (C) Lift line (D) Chord line 46. Which type of wing configuration is characterized by wings extending from the fuselage at an upward angle? (A) Anhedral (B) Dihedral (C) Cantilever (D) Gull wing 47. What is the function of the static port on an aircraft? (A) Measure static pressure (B) Measure dynamic pressure (C) Measure temperature (D) Measure altitude 48. What is the term for the upward bending of the wings of an aircraft? (A) Dihedral (B) Anhedral (C) Wing flex (D) Washout 49. What is the main purpose of the ailerons during flight? (A) Control roll (B) Decrease drag (C) Increase lift (D) Control pitch 50. Which component of an aircraft helps to reduce the tendency of the aircraft to yaw left or right? (A) Rudder (B) Vertical stabilizer (C) Ailerons (D) Elevators