WorksheetsTheory of Flight
Total questions: 14
Worksheet time: 10mins
The law which states that for every action, there is an equal and opposite reaction
Newtons 1st law
Newtons 3rd law
Bernoulli's law of fluid dynamics
Newtons 2nd law
When air flow over an airfoil ,velocity increases and pressure ....................on the top of the airfoil
Increases
Remains same
Decreases
None of the above
When the drag force become more than the thrust force ,the speed of an aircraft
It will increase
It will decrease
It will remains same
None of the above
When the speed of an aircraft is 1mach, the aircraft is traveling in
Supersonic speed
Sonic speed
Sub-sonic speed
Trims and Tabs on an aircraft are called as
Auxiliary flight control
Secondary flight control
Primary flight control
None of the above
Flaps ,Slats and Slots are called
Primary flight controls
Auxiliary flight controls
Secondary flight controls
None of above
Choose all that apply
In a steady level flight ,
Lift force = Gravity force
Thrust force = Drag force
Lift force = Thrust force
Thrust force = Gravity force
Choose all that apply, Primary flight controls include
Ailerons
Flaps
Rudder
Elevator
The axis that extends from wing tip to another wing tip is called
Longitudinal Axis
Vertical Axis
Lateral Axis
Normal Axis
The movement of aircraft in the longitudinal axis is
Pitch
Roll
Yaw
None of the above
The primary flight control, which help to do, the yaw movement in the vertical axis is
Elevator
Ailerons
Rudder
None of the above
The separation of air on the top of the wing, leads to
More lift for the aircraft
Stall
More thrust for the aircraft
No effect on the aircraft
Choose all that apply ,Lift augmentation devices located on the wings are
Flaps
Winglets
Slats
Spoiler
Acrobatic aircraft have a load factor of
1.76 G to 4.40 G
3.00 G to 6.00 G
1.52 G to 3.80 G
6.00 G to 7.00 G
