What is the Total Force Exerted by the Cockpit Seat on a Climbing Jet Pilot?

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The discussion focuses on calculating the total force exerted by the cockpit seat on a climbing jet pilot, considering both acceleration and gravitational forces. Participants clarify that the normal force (N) must be calculated by considering the pilot's weight and the components of acceleration separately. The correct approach involves breaking down the forces into horizontal and vertical components, then using the Pythagorean theorem to find the resultant force. Misunderstandings arise regarding the addition of gravitational acceleration to the net acceleration, which is not appropriate for this calculation. The final force can be determined by applying the correct formulas for the normal force and its components.
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A jet aircraft is climbing at an angle of 43° above the horizontal and is also accelerating at 4.9 m/s2. What is the total force that the cockpit seat exerts on the 65 kg pilot?(Magnitude & Direction ° above the direction of motion of the plane)

This is what I have so far:
F=ma=65*4.9=318.5
Horizontal Component of this Force = 318 .5 Cos 43° = 232.9 N
Vertical Component of this Force = 318.5 Sin 43° = 217.2 N

Direction: arctan(217.2/232.9)=43°

But it said all my answers are wrong, just wondering what I am doing wrong? :confused:
 
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Remember that if the airplane were not accelerating at all, the pilot would still have weight- he is exerting his weight on the seat and the seat is, of course, applying the same force to him.
 
You should not look for the net force, but for the contact (normal) force that the seat applies on the pilot. The two forces therefore are \vec{N}, and \vec{G} which is vertical. Break them down into components and solve for each component of \vec{N}.
 
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You didnt get the force on the passenger correct

Keep in mind that what you've computed is the force on any object but you must keep in mind that the person on the plane has a mass and has a normal force perpenduclar to the surface of hte plane. You have to take thoise into account as well

P.S. this has been edited because i had answered previousl being distrtacted for a long time in the between thus i sounded contradictory :-p
 
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stunner5000pt said:
You didnt get the force on the passenger correct

Yes the horizontal and vertical components are correct so add them up(as vectors that are perpendicular to each other) to get the force on the passenger.
The direction is correct

Your first answer probably compounded all the answers being wrong

Also keep in mind that what you've computed is the force on any object but you must keep in mind that the person on the plane has a mass and has a normal force perpenduclar to the surface of hte plane. You have to take thoise into account as well
Are you contradicting yourself: saying that the force on the passenger is incorrect, but the component forces are correct?
The problem asks what it asks: the horizontal and vertical components of the normal force the seat applies on the pilot.
 
I'm also working on this problem...My given numbers are a=4.7m/s^2 angle=49degrees mass=73kg.

Wouldn't the total force that the seat exerts on the pilot be defined by finding the resultant of the following 2 acceleration vectors?:

Vertical component acceleration + gravitational acceleration:
[4.7*sin(49) + (9.8)]

and,

Horizontal component of acceleration
[4.7*cos(49)]

I get a resultant magnitude of 13.65m/s^2 (which equals 996N) at 77degrees above the horizontal (hmm :confused: doesn't seem right at all.) Please Help.
 
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Fanman22 said:
I'm also working on this problem...My given numbers are a=4.7m/s^2 angle=49degrees mass=73kg.

Wouldn't the total force that the seat exerts on the pilot be defined by finding the resultant of the following 2 acceleration vectors?:

Vertical component acceleration + gravitational acceleration:
[4.7*sin(49) + (9.8)]

and,

Horizontal component of acceleration
[4.7*cos(49)]

I get a resultant magnitude of 13.65m/s^2 (which equals 996N) at 77degrees above the horizontal (hmm :confused: doesn't seem right at all.) Please Help.

Why, doesn't your answer look OK? An angle of 77 degrees above the horizontal for \vec{N} seems all right, because when combined with the vertically downward \vec{G} it may well result in a net force whose angle with the horizontal is 42 degrees.

Your reasoning with accelerations is not good, because \vec{a} is the net acceleration and you cannot add g, the free fall acceleration. After all, it is not the net force that is asked, but the force that the seat applies on the pilot!

So, just reason with forces, breaking them into x and y components:

N_x = ma_x = macos\theta, and

N_y - G = ma_y = masin\theta
N_y = masin\theta + mg
N_y = m(asin\theta + g)

then, apply the Pythagorean theorem to find the magnitude of N and arctan to find the angle \phi that N makes with the horizontal.
 
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