affect of social media on youth

Total
Questions

1780

PRINCIPLES OF FLIGHT
SUBSONIC AERODYNAMICS - Basics, laws and definitions
Question

The angle between the aeroplane longitudinal axis and the chord line is the:

Choices
A
B
C
D
Ref CPL A
Question

Answers angle of incidence glide path angle angle of attack climb path angle
AND ATPL A
Assuming ISA conditions, which statement with respect to the climb is correct?

Choices
A
B
C
D
Ref CPL A
Question

At constant
At constant
At constant
At constant
AND ATPL A
Maintaining

Choices
A
B
C
D
Ref CPL A
Question

Answers lead to more prominent shockwave formation make lateral stability more critical give the aircraft an increased range reduce the aft shift of CP in the transonic range
AND ATPL A
The point about which the wing pitching moment is independent of angle of attack is called:

Choices
A
B
C
D
Ref CPL A
Question

the the the the AND
The

Choices
A

psi

Answers
TAS the Mach number decreases
Mach number the IAS increases
IAS the TAS decreases
IAS the Mach number increases

Correct
A

Correct

D

thickness/chord ratio but changing to a supercritical wing section will:

Answers pitching centre centre of gravity centre of pressure aerodynamic centre
ATPL A unit of measurement of pressure is:

Correct

C

Correct

D

Answers

Correct
A

PRINCIPLES OF FLIGHT
SUBSONIC AERODYNAMICS - Basics, laws and definitions
Question

The unit of measurement of pressure is:

B
C
D
Ref CPL A
Question

kg/m3 lb/gal kg/dm2
AND ATPL A
The unit of density is:

Choices
A
B
C
D
Ref CPL A
Question

Answers
Bar
psi kg/cm2 kg/m3
AND ATPL A
The angle of attack of a wing profile is defined as the angle between:

Choices
A
B
C
D
Ref CPL A
Question

the the the the AND
The

Choices
A
B
C
D
Ref CPL A
Question

Answers the angle that determines the magnitude of the lift force the angle between the wing chord