Theory Of Flight Flashcards

1
Q

What must forces and moments be in a level flight?

A

Forces and moments must equal 0

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2
Q

What are the conditions for steady flight?

A

Thrust = drag
Lift = weight + stabiliser lift
Sum of anticlockwise moments = sum of clockwise moments

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3
Q

A heavy aircraft is travelling at the glide ratio as a lighter aircraft, what must happen for them both to touch down at the same point?

A

The heavier aircraft must travel at a faster velocity

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4
Q

What equations are there for the Best Glide Ratio?

A

Coefficient of lift / coefficient of drag
Forward speed / downward speed
Change in horizontal distance / change in vertical distance

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5
Q

What must an aircraft need more of when it is banking?

A

Lift

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6
Q

What is load factor also known as?

A

G-load

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7
Q

Give the formula for load factor

And what assumptions must be made with this formula

A

n = L / W
Or
n = 1/cos(angle)

Assuming weight is always 1

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8
Q

How can extra lift be generated?

A

Increasing the coefficient of lift or the speed

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9
Q

What does the stall speed (turn) / stall speed (level) give you?

A

Root of the load factor

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10
Q

What do flaps do?

A

Increase the camber at the trailing edge to extend the aircrafts maximum angle of attack which generates more lift

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11
Q

What are the 4 different types of flaps?

A

Plain
Slotted
Split
Fowler

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12
Q

What does the fowler flap do?

A

Increases the wing area as well as the camber and provides up to a 90% increase in the maximum coefficient of lift

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13
Q

What do slats do?

A

Increase the camber at the leading edge which provides a high energy air path to improve boundary layer control

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14
Q

What may be necessary when stall occurs?

A

Reduce the angle of attack well below the maximum angle of attack

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15
Q

What is the diagram of load factor vs equivalent air speed known as?

A

V-n diagrams

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16
Q

What is each flight envelope dependant on?

A

Aircraft gross weight
Aircraft configuration
Applicable altitude

17
Q

What are aeroelastic limits otherwise known as?

A

Redline airspeed

18
Q

To maintain lift as it balances the weight of the aircraft during take off and landing, how is the speed reduction compensated?

A

Increasing the angle of attack and the coefficient of lift