Centripetal Force (Loop the Loop)

AI Thread Summary
The discussion focuses on calculating the apparent weight of a pilot during a loop-the-loop maneuver in a jet. Given the pilot's mass of 78.0 kg, a constant speed of 105 m/s, and a loop radius of 0.562 km, the formula used is F = m(V^2/R). The calculated force at the bottom of the loop is 1530.2 N. The apparent weight is determined by adding the gravitational force to the centripetal force experienced during the maneuver.
Kajayacht
Messages
27
Reaction score
0

Homework Statement


A pilot, whose mass is 78.0 kg, makes a loop-the-loop in a fast jet. Assume that the jet maintains a constant speed of 105 m/s and that the radius of the loop-the-loop is 0.562 km. What is the apparent weight that the pilot feels (i.e., the force with which the pilot presses against the seat) at the bottom of the loop-the-loop?


Homework Equations


F = m(V^2/R)


The Attempt at a Solution



F = 78 (105^2/562)
F = 1530.2 N
 
Physics news on Phys.org
nevermind
n = m(g + v^2/R)
 
I multiplied the values first without the error limit. Got 19.38. rounded it off to 2 significant figures since the given data has 2 significant figures. So = 19. For error I used the above formula. It comes out about 1.48. Now my question is. Should I write the answer as 19±1.5 (rounding 1.48 to 2 significant figures) OR should I write it as 19±1. So in short, should the error have same number of significant figures as the mean value or should it have the same number of decimal places as...
Thread 'A cylinder connected to a hanging mass'
Let's declare that for the cylinder, mass = M = 10 kg Radius = R = 4 m For the wall and the floor, Friction coeff = ##\mu## = 0.5 For the hanging mass, mass = m = 11 kg First, we divide the force according to their respective plane (x and y thing, correct me if I'm wrong) and according to which, cylinder or the hanging mass, they're working on. Force on the hanging mass $$mg - T = ma$$ Force(Cylinder) on y $$N_f + f_w - Mg = 0$$ Force(Cylinder) on x $$T + f_f - N_w = Ma$$ There's also...
Back
Top