Relative airflow - Study guides, Class notes & Summaries

ATP CTP Course - Final Test Questions and Answers 2022. Which of the following statements regarding energy is true? The objective in maneuvering the airplane is to manage energy so that: What is the effect on total drag if airspeed slows below L/D Max? A jet pilot flying at L/D Max will obtain best: When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of drag predominates? While already at high speed, what happens if Mach is allowed to incr...

ATPL EXAM 2024 WITH QUESTIONS AND ANSWERS. What are the forces acting on an aircraft in flight? - ANSWER Drag. Thrust. Lift and Weight What is direct lift control? - ANSWER The elevator / stabilizer provide the direct lift control. What are high lift devices? - ANSWER Trailing edge flaps. Leading edge flaps. Slots Define the two major types or Drag. - ANSWER Profile and induced drag which equals total drag What are high drag devices? - ANSWER Trailing edge flaps, spoilers, landing gear...

Exam 3: NUR 3196 (Latest Update) Pathophysiology/ Pharmacology in Nursing 1 | Complete Review with Questions and Verified Answers- Grade A -100% Correct Q: Mechanics of Breathing Answer: the mechanical aspects of inspiration and expiration involve major and accessory muscles, elastic properties of the lungs and chest wall, and resistance to airflow through the conducting airways Q: Major muscles of inspiration Answer: diaphragm and external intercostal muscles (between the...

Chord - Answer-Straight line joining leading edge to the trailing edge Camber line - Answer-Line which runs midway between upper and lower surfaces of the airfoil joint the trailing and leading edge. Camber - Answer-The measure of the curvature of the airfoil. Expressed as a percentage Angle of attack - Answer-The angle between the chord of the wing and the relative airflow Centre of pressure - Answer-Lift and drag act through the centre of pressure of the wing. The centre of pressure mov...

ATPL EXAM 2024 WITH QUESTIONS AND ANSWERS. What are the forces acting on an aircraft in flight? - ANSWER Drag. Thrust. Lift and Weight What is direct lift control? - ANSWER The elevator / stabilizer provide the direct lift control. What are high lift devices? - ANSWER Trailing edge flaps. Leading edge flaps. Slots Define the two major types or Drag. - ANSWER Profile and induced drag which equals total drag What are high drag devices? - ANSWER Trailing edge flaps, spoilers, landing gear...

Aviation Unit 3 Test 100% Solved 2024 _______ decreases at 1''Hg per 1,000 foot increase in altitude. A, Barometric pressure B, Density pressure C, True altitude D, Measured pressure altitude - Answer- Barometric Pressure What are the standard temperature and pressure values for sea level? A, 59 degrees C and 1013.2 millibars B, 15 degrees F and 29.92" Hg. C, 59 degrees C and 29.92" Hg. D, 0 degrees C and 1013.2 millibars E, 15 degrees C and 29.92" Hg. - Answer- E, 15 degrees C a...

IICRC WRT Exam Questions and Verified Answers| 100% Correct| Grade A (Latest Update) 2023/ 2024 Q: When is a drying job done? Answer: A moisture meeter indicates we have met our dry goal Q: The moisture sensor can be used to verify our drying goal has been met (True or False) Answer: False Q: Moisture sensors and IR cameras are effective tools for: Answer: quickly locating moisture in carpet and pad and establishing a wet perimeter. Q: What does a thermo...

1 AVIATION UNIT 3 TEST | QUESTIONS & ANSWERS (VERIFIED) | LATEST UPDATE | GRADED A+ _______ decreases at 1''Hg per 1,000 foot increase in altitude. A, Barometric pressure B, Density pressure C, True altitude D, Measured pressure altitude Correct Answer: Barometric Pressure What are the standard temperature and pressure values for sea level? A, 59 degrees C and 1013.2 millibars B, 15 degrees F and 29.92" Hg. C, 59 degrees C and 29.92" Hg. D, 0 degrees C and 1013.2 millibars...

ATPL - AGK SET 2 (46/91)46. Which is a purpose of wing-mounted vortex generators? A. Reduce the drag caused by supersonic flow over portions of the wing. B. Increase the onset of drag divergence and aid in aileron effectiveness at high speed. C. Break the airflow over the wing so the stall will progress from the root out to the tip of the wing. - correct answers A. Reduce the drag caused by supersonic flow over portions of the wing. 47. Which is a purpose of wing-mounted vortex generator...

kinetic energy correct answers KE= 1/2M x V^2 When an object is dropped, its gravitational potential energy is converted into this type of energy gravitational potential energy correct answers Amount of stored energy that an object has when its raised above the ground- the higher the object is moved, the more potential it has PE= M x G x H (m=mass, g=acceleration of gravity 9.8m/s^2, h=height) Simply, the force of gravity on an object by the objects height (given in Joules mostly) ...