Descent Performance in Aircraft Operations - 1 Online Exam Quiz
Descent Performance in Aircraft Operations - 1 GK Quiz. Question and Answers related to Descent Performance in Aircraft Operations - 1. MCQ (Multiple Choice Questions with answers about Descent Performance in Aircraft Operations - 1
At the back side of the drag curve the rate of change of drag is negative.
Options
A : TRUE
B : FALSE
C : -
D : -
By which of the methods the flight can be descended?
Options
A : nose down pitch
B : nose uppitch
C : nose down and elevator
D : elevator and nose up
In high subsonic mach number a value dependent wave drag is not induced.
Options
A : TRUE
B : FALSE
C : -
D : -
The flight path can be controlled by the use of __
Options
A : elevator
B : rudder
C : flaps
D : slats
The flight path gradient of descent can be increased by increasing airspeed.
Options
A : TRUE
B : FALSE
C : -
D : -
The flight path is unstable during __
Options
A : the aircraft flying at airspeed less than minimum drag speed
B : the aircraft flying at airspeed more than minimum drag speed
C : the aircraft flying at airspeed less than maximum drag speed
D : the aircraft flying at airspeed more than maximum drag speed
There are three types of drag.
Options
A : TRUE
B : FALSE
C : -
D : -
Total drag is the sum of __
Options
A : lift dependent drag and lift independent drag
B : lift dependent drag, lift independent drag and volume dependent wave drag
C : lift dependent drag and volume dependent wave drag
D : volume dependent wave drag and lift independent drag
Which of the following are the two types of lift independent drag?
Options
A : surface friction drag and profile drag
B : induced drag and profile drag
C : surface friction drag and induced drag
D : parasitic drag and induced drag
Which of the following is the correct relation between lift dependent drag, lift independent drag and drag coefficient?
Options
A : CD=CDz+KCL2
B : CD=CDz-KCL2
C : CD=CDz*KCL2
D : CD=CDz/KCL2
Aerodynamic Relationships more Online Exam Quiz
Cruising Performance - Aircraft with Mixed Power Plants
Cruising Performance - Effect of Alternative Fuel Flow Laws
Cruising Performance - Specific Air Range and Specific Endurance
Descent Performance in Aircraft Operations - 2
Effect of WAT on Cruise Performance