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

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The problem involves calculating the total force exerted by a cockpit seat on a pilot in a climbing jet aircraft. The aircraft is climbing at an angle and accelerating, which raises questions about the forces acting on the pilot, including gravitational and normal forces.

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Approaches and Questions Raised

  • Participants discuss the need to consider both the normal force and gravitational force acting on the pilot. There are attempts to break down forces into components and calculate resultant forces based on acceleration and angles.

Discussion Status

Some participants have provided guidance on focusing on the normal force rather than net force, suggesting the need to consider the pilot's weight and the forces acting perpendicular to the seat. Others are exploring different approaches to calculating the resultant force, but there is no explicit consensus on the correct method.

Contextual Notes

There are varying assumptions about the parameters of the problem, including differences in acceleration values and angles, which may affect the calculations. Participants are also questioning the validity of their approaches and the definitions of the forces involved.

wildr0id
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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 [tex]\vec{N}[/tex], and [tex]\vec{G}[/tex] which is vertical. Break them down into components and solve for each component of [tex]\vec{N}[/tex].
 
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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 [tex]\vec{N}[/tex] seems all right, because when combined with the vertically downward [tex]\vec{G}[/tex] it may well result in a net force whose angle with the horizontal is 42 degrees.

Your reasoning with accelerations is not good, because [tex]\vec{a}[/tex] 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:

[tex]N_x = ma_x = macos\theta[/tex], and

[tex]N_y - G = ma_y = masin\theta[/tex]
[tex]N_y = masin\theta + mg[/tex]
[tex]N_y = m(asin\theta + g)[/tex]

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

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