B— 6,000 pounds.
The force a hydraulic actuator can exert is determined by the area of the piston and the pressure of the fluid acting on the piston.
The effective area on the retracting side of the piston is two square inches.
2 sq. in. × 3,000 psi = 6,000 pounds of force
A— directly with pressure.
The boiling point of a liquid varies directly with the pressure above the liquid. The greater the pressure, the higher the boiling point.
C— Diffusion.
Heat can be transferred from a body having a high level of heat energy to a body having a lower level of heat energy by three methods: conduction (actual physical contact), convection (transfer through vertical currents), and radiation (transfer by electromagnetic waves).
Diffusion is not a method of heat transfer.
A— 840 foot-pounds
More information is given with this problem than is needed; therefore, it can cause confusion. The only work asked for is the amount needed to move the hoist.
The hoist is moved for a distance of 12 feet and a constant force of 70 pounds is needed to move it.
The work done to move the hoist is 12 × 70 = 840 foot-pounds.
C— Absolute humidity.
Absolute humidity is the actual amount of water in a volume of air, and it is measured in such units as grams per cubic meter.
C— Unmetered pressure, 17 PSI; metered pressure, 5 psi; atmospheric pressure, 14.7 psi.
In answering this question, we must recognize that the atmospheric pressure acts equally on both sides of the metering jet and therefore does not enter into the problem. The metering jet with the greatest pressure differential across it will have the greatest rate of flow through it.
Jet A has a pressure differential of 0.5 psi differential. Jet B has a pressure differential of 11 psi differential.
Jet C has a pressure differential of 12 psi differential.
B— 15 pounds.
This block and tackle supports the weight with four ropes, and this gives it a mechanical advantage of four.
To lift a 60-pound weight, a force of 15 pounds must be exerted on rope A.
Rope A will have to be pulled four times the distance the weight is lifted.
B— 35 parts of dry air and 65 parts of water vapor.
Water vapor is only about 5/8 as heavy as an equal volume of dry air. The more water vapor in the air, the less the air weighs.
In choice A there is 2 percent water vapor.
In choice B there is 65 percent water vapor.
In choice C there is 50 percent water vapor.
B— Relative humidity.
Relative humidity is the ratio of the amount of water vapor actually present in the atmosphere to the amount that would be present if the air were saturated at the prevailing temperature and pressure.
B— changes with a change in temperature.
The speed of sound in the atmosphere varies with the temperature of the atmosphere.
8474-1.
The speed of sound in the atmosphere is most affected by variations in which of the following?
A— Sound frequency.
B— Ambient temperature.
C— Barometric pressure.
B— Ambient temperature.
The speed of sound in the atmosphere varies with the ambient temperature of the atmosphere.
C— be reduced to one-half its original value.
The pressure of a gas in an enclosed container varies inversely as the volume of the container, if the absolute temperature of the gas remains constant.
Doubling the volume of the container will decrease the pressure of the enclosed gas to a value of one-half its original pressure.
C— remain the same.
A liquid is considered to be a noncompressible fluid. Its volume changes with a change in its temperature but it remains relatively constant as its pressure changes.
If the pressure on a confined liquid is tripled, the volume of the liquid will remain virtually the same.
B— 360 foot-pounds.
Work is the product of the amount of force applied to an object times the distance through which the force causes the object to move.
As much force is needed to hold back an object when it is being lowered as it does to raise the object.
If 120 pounds of force is needed to hold back a weight as it is lowered for 3 feet, 360 foot-pounds of work has been done.
C— High temperature with high humidity.
The true landing speed of an aircraft is determined by the density of the air.
The amount of aerodynamic lift produced by the wing of an airplane or the rotor of a helicopter is determined by several things. Among these are the shape of the airfoil, the speed of the airfoil through the air, and the density of the air. The denser the air, the lower the speed that will produce the same amount of lift.
Density of the air depends upon both its temperature and its humidity. The hotter the air, the less dense. The more water vapor in the air (the higher its humidity), the less dense the air.
An airplane will have to fly the fastest to produce the required lift under conditions of high temperature and high humidity.
B— 8,000 pounds.
The size of the line that supplies fluid to an actuating cylinder has nothing to do with the amount of force the piston in the cylinder can exert.
When a pressure of 800 psi acts on a piston with an area of 10 square inches, a force of 800 × 10 = 8,000 pounds is produced.
C— Force exerted, distance moved, and time required.
Power is the time rate of doing work.
In order to determine the amount of work done, we must know the amount of force used and the distance through which this force acted. Force times distance is equal to work.
The amount of power needed is found by dividing the amount of work done by the time used in doing the work.
To find the amount of power needed to do a job, we must know the force, the distance, and the time.
A— 40 pounds.
This is a simple mechanical advantage problem.
We roll the barrel three times as far as we lift it, so the force we must exert to roll the barrel up the inclined plane is only one third of the weight of the barrel.
We must exert a force of 40 pounds to roll a 120-pound barrel up the 9-foot inclined plane to lift it 3 feet.
B— Temperature is a measure of the kinetic energy of the molecules of any substance.
Heat is a form of energy, and temperature is a measure of the intensity of the kinetic energy of the molecules in a substance.
Heat energy, in the form of latent heat, can be added to an object or taken from it without changing its temperature. But, the temperature of an object changes directly with the amount of sensible heat put into it or taken from it.
B— The actual amount of the water vapor in a mixture of air and water.
Absolute humidity is the actual amount of water in a volume of air. It is measured in such units as grams per cubic meter.
A— dewpoint.
The temperature to which a body of air must be lowered before the water vapor in the air condenses out as visible, liquid water is called the dew point of the air.
A— not change.
The pressure exerted by a confined gas is directly proportional to its absolute temperature. If the absolute temperature is doubled, the pressure will also double.
The pressure exerted by a confined gas is inversely proportional to its volume. If its volume is doubled, the pressure will decrease to a value that is one half of the original.
If both the volume and the absolute temperature of a confined gas are doubled, the two changes will cancel each other, so the pressure of the gas will not change.
A— asymmetrical lateral control at or near stall angles of attack.
Stall strips are small triangular spoilers, or wedges, attached to the leading edge in the root area of a wing that has a tendency to stall at the tip before the root. Stalls beginning at the tip cause a loss of aileron effectiveness, and therefore lateral control, when it is most needed.
At high angles of attack, stall strips disrupt the airflow over the wing root and force it to stall before the portion of the wing ahead of the aileron.
If all or a significant part of a stall strip is missing, the stall on the affected wing will begin near the tip and decrease the effectiveness of the aileron, requiring asymmetrical lateral control at or near the stall angle of attack. More aileron deflection will be needed to raise the wing with the missing stall strip than the wing with the intact strip.
8486-1.
The purpose of stall strips on airplane wings is to
A— increase lift in the areas of installation.
B— prevent stall in the areas of installation.
C— ensure that the wing root areas stall first.
C— ensure that the wing root areas stall first.
Stall strips are small triangular spoilers, or wedges, attached to the leading edge at the root area of a wing that has a tendency to stall at the tip before the root. Stalls beginning at the tip cause a loss of aileron effectiveness, and therefore lateral control, when it is most needed.
At high angles of attack, stall strips disrupt the airflow over the wing root and force it to stall before the portion of the wing ahead of the aileron.