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A comprehensive set of aviation exam questions and answers, covering a wide range of topics related to jet engines, space exploration, and the development of commercial aviation. The questions cover key concepts such as the main components of a jet engine, the purpose of nasa's mercury and gemini missions, the impact of jet engine technology on passenger travel, and the challenges in making an operational jet engine and jet aircraft. The document also includes detailed explanations and verified solutions for each question, making it a valuable resource for students and professionals in the aviation industry. The questions are structured in a way that allows for a thorough understanding of the subject matter, and the document could be useful for preparing for exams, studying, or as a reference guide.
Typology: Exams
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1b. forces are vectors because _______________. ✔✔c. they have magnitude and direction
2b. which best describes Newton's Third Law of Motion? ✔✔b. for every action there is an equal and opposite reaction
3b. lift on a wing is most properly defined as the ___________. ✔✔c. force acting perpendicular to the relative wind
4b. true or false. the reaction of downwash causes an downward reaction according to Newton's Third Law of Motion ✔✔false
5b. which of the following is true for an airplane in steady flight? select all that apply. ✔✔a. the sum of all upward components of forces equals the sum of all downward components of forces. e. the sum of all forward components of forces equals the sum of all backward components of forces
6b. which of the following is true relative to a changing angle of attack? ✔✔b. an increase in angle of attack will decrease the pressure above the wing and increase lift.
7b. the longer path theory (or equal transit time theory) says that the molecules of air flowing over the top of a wing must travel faster than the molecules of air flowing beneath the wing in order to meet art the trailing (back) edge. what is the problem with this theory? ✔✔c. it assumes
that molecules of air arriving at the front of the wing at the same time must also arrive at the back edge of the wing at the same time.
8b. the __________ of an airplane can act as an airfoil by helping to produce stability and lift. ✔✔b. fuselage
9b. increasing an airplane's wing area will ___________. select all that apply. ✔✔b. increase drag c. increase lift
10b. if the velocity of an airplane is doubled, the lift will _________ ✔✔b. increase by a factor of 4
11b. an aircraft always stalls at the same ____________ regardless of airspeed weight, or any other factor. ✔✔b. angle of attack
12b. what safety measures do airplane designers take in regard to stalls? select all that apply ✔✔d. all of the above
13b. considering an aircraft's weight and balance, _________ is the term used to describe the line or reference plane from which all measurements of "arm" are taken ✔✔c. datum
15b. the center of gravity (CG) of an airplane is forward of its acceptable CG range ✔✔d. elevator effectiveness becomes limited creating insufficient nose-up force for landing
14b. the center of gravity of an airplane can be determined by which method. ✔✔a, dividing total moments by total weight
16b. torque effect is most pronounced under which conditions? select all that apply. ✔✔a. high power setting d. low airspeed
17b. what is an advantage of a variable-pitch propeller? ✔✔b. permits the pilot to set the propeller blade angle for the most efficient performance.
18b. as airspeed decreases in level flight below that speed for maximum lift/drag ratio, total drag of a airplane __________. ✔✔b. increases because of increased induced drag
19b. which of the following is created by the resistance of air moving across the surface of an airplane? ✔✔c. skin friction drag
20b. if airspeed is doubled while in level flight, parasite drag will become_________. ✔✔c. four times greater
21b. described two of the three ways a pilot can control lift during flight. ✔✔a pilot can control lift by changing the angle of attack by varying the pitch of the airplane using the elevator, by changing the airspeed by adjusting the power setting of the engine or by climbing or descending, or by adjusting the chamber of the wing by extending or retracting lift-enhancing devices like flaps.
22b. describe how newton's third law of motion and Bernoulli's principle explain the generation of lift by an airfoil. ✔✔according to Bernoulli's principle, when air moving over the top of a wing surface travels faster than air moving over the bottom of the wing surface, pressure above the wing is reduced, producing lift. these pressure changes cause the airflow to curve downwards, creating downwash behind the airfoil. newton's third law states that for every action there is an equal and opposite reaction, so that a downward force is met with an equal and opposite upward force. when an airfoil bends traveling across its surface downward, this action results in an equal and opposite upward force called lift.
23b. is it more desirable for the wing root or wing tip to stall first and why? ✔✔it is preferable for the wing root ton stall first. if the wingtip stalls before the root, the disrupted airflow near the wingtip can reduce aileron effectiveness to such an extent that the pilot can lose control over the roll to the aircraft as the aircraft stalls, causing a wing to drop, which in extreme cases could lead to entering a spin.
24b. explain how weight and balance of an airplane can change during flight. ✔✔an airplane's weight can change during flight by the burning of fuel or dropping of cargo. the balance of an airplane can change by the movement of passengers or the incidental shifting or sliding of luggage or cargo during flight.
25b. explain how ground effect can both help and hinder during takeoff. ✔✔ground effect can be a double edged sword on takeoff. on the positive side, it will allow an airplane to fly at a slower speed than it could outside of ground effect. this is because induced drag is reduced so less thrust is needed to produce lift. this can be used to get the airplane into the air more quickly to allow easier and faster acceleration than would be possible on the ground. on the other hand, if the aircraft lifts off at too low an airspeed because of ground effect, it may not have enough speed to fly outside of ground effect and could end up setting back onto the runway.