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The force that counteracts weight and keeps the aircraft in the air is called:
You must know these basic questions on lift and drag forces.
You must know these basic questions on lift and drag forces.
The force acting to slow the wing down as it travels through the air is called:
The force that is a result of the lift and drag of a wing added together is known as:
Lift from a correctly designed aircraft wing acts at an angle that is _________.
Drag on an aircraft wing acts at an angle that is ________.
Thrust is a force produced by the aircraft and in straight and level flight is equal to:
In straight and level flight, lift is a force produced by the aircraft and is roughly equal to:
In normal straight and level flight lift equals weight. The reason we say normal is because an aerobatic aircraft that has extremely high power to weight ratio, may have the ability to sustain altitude from thrust alone. If thrust is equal to or greater than weight then this could be possible.
In normal straight and level flight lift equals weight. The reason we say normal is because an aerobatic aircraft that has extremely high power to weight ratio, may have the ability to sustain altitude from thrust alone. If thrust is equal to or greater than weight then this could be possible.
Lift force acts through the:
In reality lift is generated all over the wing. However the centre of pressure is the net result of all that lift pressure. It is generally located around 1/4 the way back from the leading edge along the chord line. You will not need this much detail.
In reality lift is generated all over the wing. However the centre of pressure is the net result of all that lift pressure. It is generally located around 1/4 the way back from the leading edge along the chord line. You will not need this much detail.
Weight is a force that acts through the:
To remember the difference between C of G and C of P. Remember it is weight affected by gravity forcing us downwards and lift affected by pressure lifting us up.
To remember the difference between C of G and C of P. Remember it is weight affected by gravity forcing us downwards and lift affected by pressure lifting us up.
Relative airflow acts:
Stall speed is:
This is a difficult question with several reasonable answers, however you must pick the best answer.
This is a difficult question with several reasonable answers, however you must pick the best answer.
The lift force always stays:
Remember this diagram. It will let you answer several almost certain exam questions.
Remember this diagram. It will let you answer several almost certain exam questions.
The length from leading edge to trailing edge of an aircraft wing is known as:
The back edge of a wing is known as:
The curvature of a wing is also known as:
A wing with a very large span to chord ratio is said to have:
Which control surface can change the curvature of a wing?
Again another loaded question as you will get in your exams. All control surfaces technically change the curvature of a wing. However the best answer and the one we deliberately use to change the entire wing curvature is the flaps.
Again another loaded question as you will get in your exams. All control surfaces technically change the curvature of a wing. However the best answer and the one we deliberately use to change the entire wing curvature is the flaps.
If you use a control surface to increase the curvature of the wing what is the resultant force?
The flaps job is to both slow the aircraft and create lift.
The flaps job is to both slow the aircraft and create lift.
Parasitic drag is made up of:
Parasitic drag is any drag that does not produce lift.
Parasitic drag is any drag that does not produce lift.
The distance between the bottom of a wing and the top of a wing at its furthest point is known as:
Rotation around the red axis is called:
Rotation around the green axis is called:
Rotation around the blue axis is called:
Rotation around the red axis is caused by which control surface?
RA-Aus BAK Exam Progress
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