Question: The range of the aircraft is increased if the aircraft is flown at a higher than optimum altitude.
Options
A : TRUE
B : FALSE
C : -
D : -
Effect of WAT on Cruise Performance more questions
Specific fuel consumption effects the range of an aircraft.
The aircraft is taken to the level ground operating for....
The best range is obtained at 1.416 Vmd.
The flight path is calculated relative to __
The minimum drag speed in terms of equivalent airspeed is....
The relative velocity of the wind produces boundary layer close....
Which of the following factors are inversely proportional to the....
Wind is the relative velocity between the air mass and....
The curly bracket in the accelerating force represents the net....
The horizontal component of the true airspeed is ___
Aerodynamic Relationships more Online Exam Quiz
Cruising Performance - Effect of Alternative Fuel Flow Laws
Cruising Performance - Specific Air Range and Specific Endurance
Descent Performance in Aircraft Operations - 1
Descent Performance in Aircraft Operations - 2
Effect of Wind on Climb Performance and Descent Performance
Effect on the Take-off Distances of Flight Variables
Equations of Motion for Performance