b. The Boeing 737 - 800 aircraft can accelerate from rest to a take- off speed of 300 kmhr-1 in 25 seconds. Calculate in ms2 the value of this acceleration, assuming it to be constant HINT: 1km = 1000m and 1hr = 3600s. kmhr-l means km divided by hr

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Chapter1: Units, Trigonometry. And Vectors
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Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...
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b. The Boeing 737 - 800 aircraft can accelerate from rest to a take-
off speed of 300 kmhr- in 25 seconds. Calculate in ms-2 the value
of this acceleration, assuming it to be constant
HINT: 1km = 1000m and 1hr = 3600s.
kmhr means km divided by hr
C.
i. The aircraft has a mass of 6 x 104 kg. Two identical jet
engines provide a thrusting force. Calculate the magnitude of
the thrusting force needed to give the aircraft the
acceleration calculated in bart (b). Hence find the thrust
Transcribed Image Text:b. The Boeing 737 - 800 aircraft can accelerate from rest to a take- off speed of 300 kmhr- in 25 seconds. Calculate in ms-2 the value of this acceleration, assuming it to be constant HINT: 1km = 1000m and 1hr = 3600s. kmhr means km divided by hr C. i. The aircraft has a mass of 6 x 104 kg. Two identical jet engines provide a thrusting force. Calculate the magnitude of the thrusting force needed to give the aircraft the acceleration calculated in bart (b). Hence find the thrust
engines provide a fhrusting Torce. CaicuIate the magniTuae oT
the thrusting force needed to give the aircraft the
acceleration calculated in part (b). Hence find the thrust
(force) for EACH engine
ii. The thrust calculated in (i) is a theoretical value. Suggest a
reason why this thrust if applied IN PRACTICE (real life)
would NOT provide this expected acceleratior
iii. The mass of the aircraft was increased by loading additional
passengers and luggage. How could this affect the time taken
to reach take-off speed?
Transcribed Image Text:engines provide a fhrusting Torce. CaicuIate the magniTuae oT the thrusting force needed to give the aircraft the acceleration calculated in part (b). Hence find the thrust (force) for EACH engine ii. The thrust calculated in (i) is a theoretical value. Suggest a reason why this thrust if applied IN PRACTICE (real life) would NOT provide this expected acceleratior iii. The mass of the aircraft was increased by loading additional passengers and luggage. How could this affect the time taken to reach take-off speed?
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