The parameters of instantaneous speed, altitude, net engine thrust, and wind speed are given when the aircraft, which accelerates and moves at a fixed altitude of 5000 kg above, releases a load of 150 kg. In case the air friction is neglected, calculate the distance between the load and the aircraft while falling to the ground.
The parameters of instantaneous speed, altitude, net engine thrust, and wind speed are given when the aircraft, which accelerates and moves at a fixed altitude of 5000 kg above, releases a load of 150 kg. In case the air friction is neglected, calculate the distance between the load and the aircraft while falling to the ground.
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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The parameters of instantaneous speed, altitude, net engine thrust, and wind speed are given when the aircraft, which accelerates and moves at a fixed altitude of 5000 kg above, releases a load of 150 kg. In case the air friction is neglected, calculate the distance between the load and the aircraft while falling to the ground.
Transcribed Image Text:W30 m/s
mHA = 5000 kg
m, = 150 kg
VHA = 200 m/s
h=10000 m
Şekil 1.
T=10000 N
T-10000 N
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