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Ok... so I was monkeying with some basic physics... and hurt myself.
Given the formula a = (v^2 - u^2) / 2s where u is initial velocity, v is final velocity, s is distance and a is acceleration... then given the following:
Given that f = m*a where m is mass, a is acceleration and f is force...
How does an aircraft with a maximum of 8200 pounds of total engine thrust actually accomplish those figures? The figures I used are from takeoff charts for an aircraft. My mind is obviously missing something. Anyone want to show me what/where?
Given the formula a = (v^2 - u^2) / 2s where u is initial velocity, v is final velocity, s is distance and a is acceleration... then given the following:
Code:
u = 0
v = 211 fps
s = 4060 feet
a = 44511 / 8120
a = 5.48 fps^2
Given that f = m*a where m is mass, a is acceleration and f is force...
Code:
m = 20200 pounds
a = 5.48 fps^2
f = 20200 * 5.48
f = 110729 pounds
How does an aircraft with a maximum of 8200 pounds of total engine thrust actually accomplish those figures? The figures I used are from takeoff charts for an aircraft. My mind is obviously missing something. Anyone want to show me what/where?





