Question 2

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Question 5:

An aircraft climbs at an angle of 15°. The

weight of the aircraft is 115 kN and its wing

area is 78 m². The aircraft's drag equation is

given by CD 0.035 0.025 C². If the

engines of the aircraft produce 47 kN of thrust

during the climb what is the fastest equivalent

airspeed the aircraft could be climbing at? The

answer should have units of m s´¹.

Question 3

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2 pts

Question 6:

The thrust required for a cargo aircraft to fly

straight, leveld steady we

ured. In each