Effect of WAT on Cruise Performance Online Exam Quiz
Effect of WAT on Cruise Performance GK Quiz. Question and Answers related to Effect of WAT on Cruise Performance. MCQ (Multiple Choice Questions with answers about Effect of WAT on Cruise Performance
It is assumed zero velocity datum at the aerodynamic center of the aircraft.
Options
A : TRUE
B : FALSE
C : -
D : -
Specific fuel consumption effects the range of an aircraft.
Options
A : TRUE
B : FALSE
C : -
D : -
The aircraft is taken to the level ground operating for __
Options
A : considering vertical component of the wind
B : considering horizontal component of the wind
C : considering both horizontal and vertical component of the wind
D : neglecting the effect of wind
The best range is obtained at 1.416 Vmd.
Options
A : TRUE
B : FALSE
C : -
D : -
The flight path is calculated relative to __
Options
A : air mass
B : still air condition
C : air mass and still air condition
D : airspeed
The minimum drag speed in terms of equivalent airspeed is unaffected by the altitude.
Options
A : TRUE
B : FALSE
C : -
D : -
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 : -
The relative velocity of the wind produces boundary layer close to the ground which ___
Options
A : decreases the wind speed with decrease in height
B : increases the wind speed with decrease in height
C : makes the wind speed unaffected
D : constantly increases
Which of the following factors are inversely proportional to the range of the aircraft?
Options
A : Altitude
B : Ambient relative pressure
C : Temperature
D : Mach number
Wind is the relative velocity between the air mass and the ground.
Options
A : TRUE
B : FALSE
C : -
D : -
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Effect of Wind on Climb Performance and Descent Performance
Effect on the Take-off Distances of Flight Variables
Equations of Motion for Performance