, Which of the following statements regarding energy is true
II d. Kinetic energy can be
II II II II II II II II II II II II II II
traded for potential energy, and potential energy can be traded for kinetic energy
II II II II II II II II II II II II II
The objective in maneuvering the airplane is to manage energy so that: d. All of the
II II II II II II II II II II II II II II II II II II
above
II
What is the effect on total drag if airspeed slows below /
II II II II II II II II II II II II II II II II c. rag increases II II
because of increased induced drag.
II II II II II
II A jet pilot flying at L/D Max will obtain best: - b. Endurance
II II II II II II II II II II II II II
When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of
II II II II II II II II II II II II II II II II
drag predominate
II a. Parasite
II II II II II
While already at high speed, what happens if
II II II II II II II II II is allowed to increase
II II II II II d. All of the
II II II II II
above
II
II What is the result of a shock-induced separation of airflow occurring symmetrically near
II II II II II II II II II II II II
II the wing root of a swept wing aircraft c. A severe moment of "Mach tuck"
II II II II II II II II II II II II II II II II
The speed of sound generally decreases with increasing altitude. This occurs because:
II II II II II II II II II II II II II II
a. The air temperature decreases.
II II II II II
II ritical number can be defined as: c. The speed of an aircraft in which airflow over
II II II II II II II II II II II II II II II II II II
II any part of the aircraft or structure first reaches, but doesn't exceed
II II . . II II II II II II II II II II II
II Stability in the vertical axis tends to drive the sideslip angle toward zero. The most
II II II II II II II II II II II II II II
II dynamic stability about the vertical axis on modern jet transports is from: c. An active
II II II II II II II II II II II II II II II II
II stability augmentation system / yaw damper. II II II II II
II Swept wings cause a significant: - b. Reduction in effectiveness of flaps.
II II II II II II II II II II II II
II Why is convergence of Stall AOA and Mmo hazardous? - d. All of the above
II II II II II II II II II II II II II II II
To maintain altitude in a banked turn, the lift produced by the airplane must be: a.
II II II II II II II II II II II II II II II II II II
Greater than the airplane weight, and the amount is a function of bank angle.
II II II II II II II II II II II II II II
II Excessive bank angles at high altitudes can be hazardous because: - d. All of the above II II II II II II II II II II II II II II II II
II When operating at constant speed with constant thrust setting at high altitude
II II II II II II II II II II II II
II above F in slow flight below / airspeed, any disturbance causing a decrease
II II II II II II II II II II II II II
II d. Kinetic energy can be
II II II II II II II II II II II II II II
traded for potential energy, and potential energy can be traded for kinetic energy
II II II II II II II II II II II II II
The objective in maneuvering the airplane is to manage energy so that: d. All of the
II II II II II II II II II II II II II II II II II II
above
II
What is the effect on total drag if airspeed slows below /
II II II II II II II II II II II II II II II II c. rag increases II II
because of increased induced drag.
II II II II II
II A jet pilot flying at L/D Max will obtain best: - b. Endurance
II II II II II II II II II II II II II
When a jet aircraft is flown at the appropriate airspeed for maximum range, which type of
II II II II II II II II II II II II II II II II
drag predominate
II a. Parasite
II II II II II
While already at high speed, what happens if
II II II II II II II II II is allowed to increase
II II II II II d. All of the
II II II II II
above
II
II What is the result of a shock-induced separation of airflow occurring symmetrically near
II II II II II II II II II II II II
II the wing root of a swept wing aircraft c. A severe moment of "Mach tuck"
II II II II II II II II II II II II II II II II
The speed of sound generally decreases with increasing altitude. This occurs because:
II II II II II II II II II II II II II II
a. The air temperature decreases.
II II II II II
II ritical number can be defined as: c. The speed of an aircraft in which airflow over
II II II II II II II II II II II II II II II II II II
II any part of the aircraft or structure first reaches, but doesn't exceed
II II . . II II II II II II II II II II II
II Stability in the vertical axis tends to drive the sideslip angle toward zero. The most
II II II II II II II II II II II II II II
II dynamic stability about the vertical axis on modern jet transports is from: c. An active
II II II II II II II II II II II II II II II II
II stability augmentation system / yaw damper. II II II II II
II Swept wings cause a significant: - b. Reduction in effectiveness of flaps.
II II II II II II II II II II II II
II Why is convergence of Stall AOA and Mmo hazardous? - d. All of the above
II II II II II II II II II II II II II II II
To maintain altitude in a banked turn, the lift produced by the airplane must be: a.
II II II II II II II II II II II II II II II II II II
Greater than the airplane weight, and the amount is a function of bank angle.
II II II II II II II II II II II II II II
II Excessive bank angles at high altitudes can be hazardous because: - d. All of the above II II II II II II II II II II II II II II II II
II When operating at constant speed with constant thrust setting at high altitude
II II II II II II II II II II II II
II above F in slow flight below / airspeed, any disturbance causing a decrease
II II II II II II II II II II II II II
