a. Triple
b. Be reduced to one third its original volume
c. Remain the same
c. Remain the same
a. Low temperature with low humidity
b. High temperature with low humidity
c. High temperature with high humidity
c. High temperature with high humidity
a. Increase the lift to drag ratio
b. reduce the aspect ratio
c. Optimize wing dihedral and improve lateral stability
a. Increase the lift to drag ratio
a. Unmetered pressure, 18 PSI; metered pressure, 17.5 PSI; atmospheric pressure 14.5 PSI
b. Unmetered pressure, 23 PSI; metered pressure, 12 PSI; atmospheric pressure 14.3 PSI
c. Unmetered pressure, 17 PSI; metered pressure, 5 PSI; atmospheric pressure, 14.7 PSI
c. Unmetered pressure, 17 PSI; metered pressure, 5 PSI; atmospheric pressure, 14.7 PSI
a. 9,000 pounds
b. 6,000 pounds
c. 3,000 pounds
b. 6,000 pounds
a. To every action is an equal and opposite reaction
b. Force is proportional to the product of mass and acceleration
c. Everybody persists in its state of rest, or of motion in a straight line, unless acted upon by some force.
c. Everybody persists in its state of rest, or of motion in a straight line, unless acted upon by some force.
a. Wingspan to the wing root
b. Square of the chord to the wingspan
c. Wingspan to the mean chord
c. Wingspan to the mean chord
a. 840 foot pounds
b. 1,890 foot pounds
c. 1,050 foot pounds
a. 840 foot pounds
a. 1 and 2
b. 2 and 3
c. 1,2 and 3
c. 1,2 and 3
a. Sound frequency (cps)
b. Ambient temperature
c. Barometric pressure
b. Ambient temperature
a. The temperature to which humid air must be cooled at constant pressure to become statured.
b. The actual amount of the water vapor in a mixture of air and water.
c. The ratio of the 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. The actual amount of water vapor in a mixture of air and water.
a. Asymmetrical lateral control at a near stall angles of attack
b. Decreased lift in the area of installation at high angles
c. Asymmetrical lateral control at low angles of attack.
a. Asymmetrical lateral control at a near stall angles of attack
a. Increase in direct proportion to the volume increase
b. Remain the same
c. Be reduced to one half its original value
c. Be reduced to one half its original value
a. A positive air pressure below and above the wing’s surface along with the downward deflection of air
b. Positive air pressure below the wing’s surface and negative air pressure above the wing’s surface along with the downward deflection of air.
c. Negative air pressure below the wing’s surface and positive air pressure above the wing’s surface along with the downward deflection of air.
b. Positive air pressure below the wing’s surface and negative air pressure above the wing’s surface along with the downward deflection of air.
a. Increase lateral stability
b. Increase longitudinal stability
c. Increase lift coefficient of the wing
a. Increase lateral stability
a. Not change
b. Be halved
c. Become four times as great
a. Not change
a. Directly with pressure
b. Inversely with pressure
c. Directly with density
a. Directly with pressure
a. Dew point
b. Absolute humidity
c. Relative humidity
a. Dew point
a. Varies according to the frequency of the sound
b. Changes with a change in temperature
c. Changes with a change in pressure
b. Changes with a change in temperature
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
a. There is an inverse relationship between temperature and heat
b. Temperature is a measure of the kinetic energy of the molecules of any substance
c. Temperature is a measure of the potential energy of the molecules of any substance
b. Temperature is a measure of the kinetic energy of the molecules of any substance
a. Convection
b. Conduction
c. Diffusion
c. Diffusion
a. Increased drag at high angles of attack
b. A low stall speed
c. Poor control qualities at low airspeeds
b. A low stall speed
a. 120 pounds of force
b. 360 foot-pounds
c. 40 foot-pounds
b. 360 foot-pounds