Question: 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
Effect of WAT on Cruise Performance more questions
What is the relation between air temperature and the aircraft....
What is the relation between altitude and the aircraft range?
Which of the following is a correct statement?
It is assumed zero velocity datum at the aerodynamic center....
Specific fuel consumption effects the range of an aircraft.
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 range of the aircraft is increased if the aircraft....
The relative velocity of the wind produces boundary layer close....
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