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AERT 4040 Final Exam UPDATED QUESTIONS AND CORRECT ANSWERS

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AERT 4040 Final Exam UPDATED QUESTIONS AND CORRECT ANSWERS Intro Quiz - CORRECT ANSWER The Critical Mach Number of an aircraft is the highest Mach Number the aircraft can travel before structural damage is done to the airframe. - CORRECT ANSWER False How did the Wrights correct their problem of roll reversal? - CORRECT ANSWER They developed a movable rudder and connected it to the roll control The temperature and pressure conditions for a standard day are ______________. - CORRECT ANSWER 59 degrees F / 15 degrees C and 29.92 in of Hg / 1013 mbar Density is - CORRECT ANSWER Mass per unit volume What did the Wright brothers think was the most difficult problem, thus the first problem they attacked when building their Flyer? - CORRECT ANSWER How to control and balance the aircraft What was unique about the engine that the Wrights used for their Flyer? - CORRECT ANSWER It was the first time aluminum was used in the construction od an aircraft Density Altitude is used as a predictor of aircraft performance, not as a height reference. - CORRECT ANSWER True

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AERT 4040 Final Exam UPDATED
QUESTIONS AND CORRECT ANSWERS
Intro Quiz - CORRECT ANSWER



The Critical Mach Number of an aircraft is the highest Mach Number the aircraft can travel
before structural damage is done to the airframe. - CORRECT ANSWER False



How did the Wrights correct their problem of roll reversal? - CORRECT
ANSWER They developed a movable rudder and connected it to the roll control



The temperature and pressure conditions for a standard day are ______________. -
CORRECT ANSWER 59 degrees F / 15 degrees C and 29.92 in of Hg / 1013 mbar



Density is - CORRECT ANSWER Mass per unit volume



What did the Wright brothers think was the most difficult problem, thus the first problem they
attacked when building their Flyer? - CORRECT ANSWER How to control and
balance the aircraft



What was unique about the engine that the Wrights used for their Flyer? - CORRECT
ANSWER It was the first time aluminum was used in the construction od an aircraft



Density Altitude is used as a predictor of aircraft performance, not as a height reference. -
CORRECT ANSWER True



What method did the Wright brothers use to control roll? - CORRECT ANSWER They
developed a technique of wing warping



The speed of sound in air is dependent upon the - CORRECT ANSWER Air
Temperature only

,Air viscosity __________ as the air temperature increases. - CORRECT
ANSWER Increases



An aircraft's Mach Number is the aircraft's - CORRECT ANSWER TAS divided by the
Local Speed of Sound



The Basics Quiz - CORRECT ANSWER



The chord of an airfoil is defined as ___________. - CORRECT ANSWER a measure
of the wing along the chord line, from the leading edge to the trailing edge



Aspect Ratio of a wing is - CORRECT ANSWER the ratio of the wingspan to the
average cord



A moment is _________. - CORRECT ANSWER created when a force is applied at
some distance from an axis or fulcrum, producing rotation about that point



Total pressure is: - CORRECT ANSWER static pressure plus dynamic pressure



The center of gravity is the point at which __________. - CORRECT ANSWER all
weight is concentrated



Wing Loading is: - CORRECT ANSWER the ratio of the aircraft weight to the surface
area of the wing



The camber of an airfoil: - CORRECT ANSWER is the maximum distance between
the cord and the mean camber line measured perpendicular to the cord


The angle of attack of a wing is the angle between the wing's cord and the horizon -
CORRECT ANSWER False

, The Law of Interaction states __________. - CORRECT ANSWER "For every action
there is an equal and opposite reaction."



The General Gas Law sets the relationship between three properties of air: pressure (P),
density (ρ), and temperature (T). It is expressed as an equation where R is a constant for any
given gas. What is the correct expression of the General Gas Law. - CORRECT
ANSWER ρ = P/RT



The angle of incidence of a wing is the angle between a line drawn through the 25% cord
points and a line drawn parallel to the lateral axis. - CORRECT ANSWER False



The axis is which the aircraft nose moves left or right about the center of gravity. -
CORRECT ANSWER yaw



Static pressure acts: - CORRECT ANSWER in all directions



Which formula or equation describes the relationship between force (F), acceleration (a) and
mass (m)? - CORRECT ANSWER F = ma



The Mean Camber Line: - CORRECT ANSWER is a line drawn halfway between the
upper and lower surface of an airfoil.



Lift Quiz - CORRECT ANSWER



A _________ airfoil produces lift at zero degrees angle of attack. - CORRECT
ANSWER positively cambered



When an aircraft flies more slowly, more AOA is needed, when it flies faster less AOA is
needed - CORRECT ANSWER True

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