L8 - Static Directional and Lateral Stability Flashcards

1
Q

Define Static Directional Stability?

A

The ability of an aircraft to resist slipping.

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2
Q

What component mainly determines directional stability?

A

Vertical Tail

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3
Q

What direction is positive slideslip angle?

A

From a top down view, anticlockwise

Wind in right ear

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4
Q

What is the condition for aircraft static directional stability?

A

dCn/d(Beta) > 0

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5
Q

How does dihedral increase lateral stability?

A

Once disturbed, a velocity component caused by sideslip is introduced. Dihedral wings means that the lower wing has a higher angle of attack, producing more lift, creating a moment and stabalising the aircraft.

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6
Q

What is the condition for aircraft static lateral stability?

A

dCl/d(Beta) < 0

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7
Q

Define manoeuvre?

A

A change of one state of flight to another state of

flight, with a change in the acceleration.

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8
Q

What are the 4 main longitudinal manoeuvres?

A

Pull up
Push over
Rollercoaster
Loop

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9
Q

What is the opposition of manoeuverability?

A

Static stability.

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10
Q

What is Manoeuvre stability?

A

the force that needs to be

applied on the stick to change the g-load

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11
Q

What is manoeuverability usually measured in?

A

Stick force per g.

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12
Q

What is the condition for longitudinal manoeuvre stability?

A

dC’m/dC’l < 0

Desh signifies inclusion of pitch rate term.

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13
Q

What is usually more aft? Stick free of Stick fixed points?

A

Stick fixed.

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14
Q

What factors affect lateral stability?

A

– Wing dihedral angle
– Wing sweepback angle
– Fuselage – wing position, e.g. high wing
– High vertical tail

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15
Q

What has a higher centre of gravity? High or low wing?

A

Low wing has higher centre of gravity.

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