Precarious Lunch
A uniform steel beam of length and mass is bolted to the side of a building. The beam is supported by a steel cable attached to the end of the beam at an angle , as shown. The wall exerts an unknown force, , on the beam. A workman of mass sits eating lunch a distance from the building.

  1. Find , the tension in the cable. Remember to account for all the forces in the problem.
    Express your answer in terms of , , , , , and , the magnitude of the acceleration due to gravity.

= / g*(m_1*L/2+m_2*d)/(L*sin(theta))
  1. Find , the x-component of the force exerted by the wall on the beam (), using the axis shown. Remember to pay attention to the direction that the wall exerts the force.
    Express your answer in terms of and other given quantities.

= / -T*cos(theta)
  1. Find , the y-component of force that the wall exerts on the beam (), using the axis shown. Remember to pay attention to the direction that the wall exerts the force.
    Express your answer in terms of , , , , and .

= / -sin(theta)*T+m_1*g+m_2*g

[Print]

Sliding Dresser
Sam is trying to move a dresser of mass and dimensions of length and height by pushing it with a horizontal force applied at a height above the floor. The coefficient of kinetic friction between the dresser and the floor is and is the magnitude of the acceleration due to gravity. The ground exerts upward normal forces of magnitudes and at the two ends of the dresser. Note that this problem is two dimensional.

  1. If the dresser is sliding with constant velocity, find , the magnitude of the force that Sam applies.
    Express the force in terms of , , and .

= / mu_k*m*g
  1. Find the magnitude of the normal force . Assume that the legs are separated by a distance , as shown in the figure.
    Express this normal force in terms of , , , , and .

= / m*g/2-mu_k*m*g*h/L
  1. Find the magnitude of the normal force . Assume that the legs are separated by a distance , as shown in the figure.
    Answer in terms of , , , , and .

= / m*g/2+mu_k*m*g*h/L
  1. Find , the maximum height at which Sam can push the dresser without causing it to topple over.
    Express your answer for the maximum height in terms and .

= / L/(2*mu_k)

A Person Standing on a Leaning Ladder
A uniform ladder with mass and length rests against a smooth wall. A do-it-yourself enthusiast of mass stands on the ladder a distance from the bottom (measured along the ladder). The ladder makes an angle with the ground. There is no friction between the wall and the ladder, but there is a frictional force of magnitude between the floor and the ladder. is the magnitude of the normal force exerted by the wall on the ladder, and is the magnitude of the normal force exerted by the ground on the ladder. Throughout the problem, consider counterclockwise torques to be positive. None of your answers should involve (i.e., simplify your trig functions).

  1. What is the minimum coeffecient of static friction required between the ladder and the ground so that the ladder does not slip?
    Express in terms of , , , , and .

= / (m_1*d+m_2*L/2)*cos(theta)/((m_1+m_2)*L*sin(theta))
  1. Suppose that the actual coefficent of friction is one and a half times as large as the value of . That is, . Under these circumstances, what is the magnitude of the force of friction that the floor applies to the ladder?
    Express your answer in terms of , , , , , and . Remember to pay attention to the relation of force and .

= / (m_1*d+m_2*L/2)*cos(theta)*g/(L*sin(theta))

Three-Legged Table
The top view of a table, with weight , is shown in the figure. The table has lost the leg at (, ), in the upper right corner of the diagram, and is in danger of tipping over. Company is about to arrive, so the host tries to stabilize the table by placing a heavy vase (represented by the green circle) of weight at (, ). Denote the magnitudes of the upward forces on the table due to the legs at (0, 0), (, 0), and (0, ) as , , and , respectively.

  1. Find , the magnitude of the upward force on the table due to the leg at (, 0).
    Express the force in terms of , , , , , and/or . Note that not all of these quantities may appear in the answer.

= / W_v*X/L_x + W_t/2
  1. Find , the magnitude of the upward force on the table due to the leg at (0, ).
    Express the force in terms of , , , , , and/or . Note that not all of these quantities may appear in the final answer.

= / W_v*Y/L_y+W_t/2
  1. Find , the magnitude of the upward force on the table due to the leg at (0, 0).
    Express the force in terms of , , , , , , , and/or . Note that not all terms may appear in the answer.

= / W_v*(1-X/L_x-Y/L_y)

While the host is greeting the guests, the cat (of weight ) gets on the table and walks until her position is .

  1. Find the maximum weight of the cat such that the table does not tip over and break the vase.
    Express the cat's weight in terms of , , , , and .

= / W_v*(1-X/L_x-Y/L_y)

Young's Modulus
Learning Goal: To understand the meaning of Young's modulus, to perform some real-life calculations related to stretching steel, a common construction material, and to introduce the concept of breaking stress.
You are aready familiar with Hooke's law, which states that for springs and other "elastic" objects

,

where is the magnitude of the stretching force, is the corresponding elongation of the spring from equilibrium, and is a constant that depends on the geometry and the material of the spring. If the deformations are small enough, most materials, in fact, behave like springs: Their deformation is directly proportional to the external force. Therefore, it may be useful to operate with an expression that is similar to Hooke's law but describes the properties of various materials, as opposed to various objects such as springs. Such an expression does exist. Consider, for instance, a bar of initial length and cross-sectional area stressed by a force of magnitude . As a result, the bar stretches by .

Let us define two new terms:

  • Tensile stress is the ratio of the stretching force to the cross-sectional area:

.

  • Tensile strain is the ratio of the elongation of the rod to the initial length of the bar:

.

It turns out that the ratio of the tensile stress to the tensile strain is a constant--as long as the tensile stress is not too large. That constant, which is an inherent property of a material, is called Young's modulus and is given by

  1. What is the SI unit of Young's modulus?

Pa
or
pascal
or
Pascal
or
pascals
or
Pascals
or
kg/(m*s^2)
or
N/(m^2)
  1. Consider a metal bar of initial length and cross-sectional area . The Young's modulus of the material of the bar is . Find the "spring constant" of such a bar for low values of tensile strain.
    Express your answer in terms of , , and .

= / Y*A/L
  1. Ten identical steel wires have equal lengths and equal "spring constants" . The wires are connected end to end, so that the resultant wire has the length of . What is the "spring constant" of the resulting wire?
  1. Ten identical steel wires have equal lengths and equal "spring constants" . The wires are slightly twisted together, so that the resultant wire has the length of and is ten times as thick as the individual wire. What is the "spring constant" of the resulting wire?
  1. Ten identical steel wires have equal lengths and equal "spring constants" . The Young's modulus of each wire is . The wires are connected end to end, so that the resultant wire has the length of . What is the Young's modulus of the resulting wire?
  1. Ten identical steel wires have equal lengths and equal "spring constants" . The Young's modulus of each wire is . The wires are slightly twisted together, so that the resultant wire has the length of and is ten times as thick as the individual wire. What is the Young's modulus of the resulting wire?
  1. Consider a steel guitar string of initial length and cross-sectional area . The Young's modulus of steel is . How far () would such a string stretch under a tension of 1500 N?
    Use two significant figures in your answer. Express your answer in millimeters.

= / 15
/ mm
  1. Although humans have been able to fly hundreds of thousands of miles into outer space, getting inside the earth has proven much more difficult. The deepest mines ever drilled are only about 10 miles deep. To illustrate the difficulties associated with such drilling, consider the following: The density of steel is about and its breaking stress--defined as the maximum stress the material can bear without deteriorating--is about . What is the maximum length of a steel cable that can be lowered into a mine? Assume that the magnitude of the acceleration due to gravity remains constant at .
    Use two significant figures in your answer. Express your answer in kilometers.

26
/ km

Escape Velocity
Learning Goal: To introduce you to the concept of escape velocity for a rocket.
The escape velocity is defined to be the minimum speed with which an object of mass must move to escape from the gravitational attraction of a much larger body, such as a planet of total mass . The escape velocity is a function of the distance of the object from the center of the planet , but unless otherwise specified this distance is taken to be the radius of the planet because it addresses the question "How fast does my rocket have to go to escape from the surface of the planet?"

  1. The key to making a concise mathematical definition of escape velocity is to consider the energy. If an object is launched at its escape velocity, what is the total mechanical energy of the object at a very large (i.e., infinite) distance from the planet? Follow the usual convention and take the gravitational potential energy to be zero at very large distances.

= / 0

Consider the motion of an object between a point close to the planet and a point very very far from the planet. Indicate whether the following statements are true or false.

  1. Angular momentum about the center of the planet is conserved.

true false
  1. Total mechanical energy is conserved.

true false
  1. Kinetic energy is conserved.

true false
  1. The angular momentum about the center of the planet and the total mechanical energy will be conserved regardless of whether the object moves from small to large (like a rocket being launched) or from large to small (like a comet approaching the earth).

true false
  1. Find the escape velocity for an object of mass that is initially at a distance from the center of a planet of mass . Assume that , the radius of the planet, and ignore air resistance.
    Express the escape velocity in terms of , , , and , the universal gravitational constant.

= / (2*G*M/R)^(1/2)

[Print]

Properties of Circular Orbits
Learning Goal: To teach you how to find the parameters characterizing an object in a circular orbit around a much heavier body like the earth.

The motivation for Isaac Newton to discover his laws of motion was to explain the properties of planetary orbits that were observed by Tycho Brahe and analyzed by Johannes Kepler. A good starting point for understanding this (as well as the speed of the space shuttle and the height of geostationary satellites) is the simplest orbit--a circular one. This problem concerns the properties of circular orbits for a satellite orbiting a planet of mass .

For all parts of this problem, where appropriate, use for the universal gravitational constant.

  1. Find the orbital speed for a satellite in a circular orbit of radius .
    Express the orbital speed in terms of , , and .

= / sqrt(G*M/R)
  1. Find the kinetic energy of a satellite with mass in a circular orbit with radius .
    Express your answer in terms of , , , and .

= / G*M*m/(2*R)
  1. Express the kinetic energy in terms of the potential energy .

= / -1/2*U
  1. Find the orbital period .
    Express your answer in terms of , , , and .

= / 2*pi*R^(3/2)*(G*M)^(-1/2)
  1. Find an expression for the square of the orbital period.
    Express your answer in terms of , , , and .

= / (2*pi)^2/(G*M)* R^3
  1. Find , the magnitude of the angular momentum of the satellite with respect to the center of the planet.
    Express your answer in terms of , , , and .

= / m*(G*M*R)^0.5
  1. The quantities , , , and all represent physical quantities characterizing the orbit that depend on radius . Indicate the exponent (power) of the radial dependence of the absolute value of each.
    Express your answer as a comma-separated list of exponents corresponding to , , , and , in that order. For example, -1,-1/2,-0.5,-3/2 would mean , , and so forth.

-1/2 / , / -1 / , / -1 / , / 1/2

Geosynchronous Satellite
A satellite that goes around the earth once every 24 hours is called a geosynchronous satellite. If a geosynchronous satellite is in an equatorial orbit, its position appears stationary with respect to a ground station, and it is known as a geostationary satellite.

  1. Find the radius of the orbit of a geosynchronous satellite that circles the earth. (Note that is measured from the center of the earth, not the surface.)
    You may use the following constants:
  2. The universal gravitational constant is .
  3. The mass of the earth is .
  4. The radius of the earth is .

Give the orbital radius in meters to three significant digits.

= / 4.225*10^7 (+/- 0.2%)
or
(5.98*10^24*6.67*10^-11 /(2*pi/(24*60*60))^2)^(1/3)
/ m

[Print]

A Satellite with Drag

This problem concerns the properties of circular orbits for a satellite of mass orbiting a planet of mass in an almost circular orbit of radius .

In doing this problem, you are to assume that the planet has an atmosphere that causes a small drag due to air resistance. "Small" means that there is little change during each orbit so that the orbit remains nearly circular, but the radius can change slowly with time.

The following questions will ask about the net effects of drag and gravity on the satellite's motion, under the assumption that the satellite's orbit stays nearly circular. Use if necessary for the universal gravitational constant.

  1. The total mechanical energy of the satellite will ______.

increase
decrease
stay the same
vary in a more complex way than is listed here
  1. What is the potential energy of the satellite?
    Express your answer in terms of , , , and .

= / -m*M*G/r
  1. What is the kinetic energy of the satellite?
    Express the kinetic energy in terms of , , , and .

= / 1/2*m*M*G/r
  1. As the force of the air resistance acts on the satellite, the radius of the satellite's orbit will ______.

increase
decrease
stay the same
vary in a more complex way than is listed here
  1. As the force of the air resistance acts on the satellite, the kinetic energy of the satellite will ______.

increase
decrease
stay the same
vary in a more complex way than is listed here
  1. Which force or forces lead to a change in kinetic energy? That is, which force or forces do work on the satellite?

gravity alone
the drag force alone
both the drag force and gravity
  1. As the force of the air resistance acts on the satellite, the magnitude of the angular momentum of the satellite with respect to the center of the planet will ______.

increase
decrease
stay the same
vary in a more complex way than is listed here
  1. Which force or forces will cause the magnitude of the satellite's angular momentum with respect to the center of the planet to change?

gravity alone
the drag force alone
both the drag force and gravity

Post-Collision Orbit

A small asteroid is moving in a circular orbit of radius about the sun. This asteroid is suddenly struck by another asteroid. (We won't worry about what happens to the second asteroid, and we'll assume that the first asteroid does not acquire a high enough velocity to escape from the sun's gravity). Immediately after the collision, the speed of the original asteroid is , and it is moving at an angle relative to the radial direction, as shown in the figure. Assume that the mass of the asteroid is and that the mass of the sun is , and use for the universal gravitation constant.

Since the asteroid does not reach escape velocity, it must remain in a bound orbit around the sun, which will be an ellipse. Take the following steps to find and , the aphelion and perihelion distance of the asteroid after the collision. (The aphelion is the point in the orbit farthest from the sun, and the perihelion is the point in the orbit closest to the sun.)

As in most orbit problems, the most fundamental principles involved are energy and angular momentum conservation.

  1. What is the total energy of the asteroid immediately after the collision?
    Express the total energy in terms of , , , , , and .

= / 0.5*m*V_0^2-G*M*m/R_0
  1. What is , the magnitude of the angular momentum of the asteroid immediately after the collision, as measured about the center of the sun?
    Express the magnitude of the angular momentum in terms of , , , , , and .

= / m*V_0*R_0*sin(theta)

, , and are given initial conditions, and the values of , , and are known constants. The total energy and angular momentum may be expressed entirely in terms of these known, fixed quantities. This means that we should be able to express any of the fixed quantities related to the new orbit in terms of , , and known constants, instead of using the initial conditions.