Flight Controls | Aeroelasticity Flashcards

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1
Q

Aeroelasticity is the ___, or ___

A
  • interaction between aerodynamic loads and elastic strain on the airframe
  • Whether a component bends or twists under the loads imposed by flight
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2
Q

A material is said to be wholly elastic if ___

A

The strain caused by a stress goes away when the stress is removed

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3
Q

A material is said to be plastic when ___

A

The strain caused by a stress does not go away when removed

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4
Q

The new position of a plastic material following an applied stress is called the ___

A

permanent set

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5
Q

___ wings and surfaces with ___ aspect ratios will suffer the most from aeroelastic distortion

A

Swept high

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6
Q

Flutter is a ___

A

divergent oscillatory motion of a control surface from the interaction of aerodynamic and inertia forces, and stiffness of the structure

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7
Q

Flexural flutter is caused by ___

A

CG of a control surface being offset from the control hinge line, with flex as lift changes.

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8
Q

Flexural flutter can be prevented by ___

A

introducing mass balances in front of the torsion axis to better place the CG

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9
Q

Torsional flutter is aka ___ ___

A

cyclic deformation

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10
Q

Torsional flutter will occur when ___

A

increased lift on a control surface causes a turning moment about a torsional axis

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11
Q

Buffeting is ___

A

high-frequency instabiliy caused by airflow separation of shock wave oscillations from one object striking another

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12
Q

During divergence, elastic twist suddenly becomes ___

A

infinite

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13
Q

Fly-by-wire systems use ___ transmitted over ___ that connect to ___ at the control surfaces

A

electrical systems, electrical cables, hydraulic actuators

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14
Q

With fly by wire, the flight controls operate ___ in the shape of ____ which produce command signals based on the voltages that are proportional to the movement of the control

A

transducers, Rotary Variable Differential Transformers

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15
Q

The benefits of Fly By Wire are ___

A
  • Save weight
  • Reduce maintenance
  • Save space
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16
Q

Fly by wire redundency is achieved by having ___ or ___

A

multiple pathways for signals, or multiple computers for the same task

17
Q

Flight control software is certified to the highest level: _

A

A

18
Q

Software levels are designed according to the ___

A

effects of a software failure

19
Q

Reversible flight controls must have a ___ which are essential for manual controls

A

gust lock

20
Q

On a cable operated system, the gust lock will stop the control column from moving if the controls do not have ___ ___

A

servo tabs

21
Q

Primary stops are fitted to ___

A

control surfaces

22
Q

Secondary stops are fitted to ___

A

flight controls

23
Q

TOCWS is ___

A

Take Off Configuration Warning System

24
Q

Aileron upset is a system that biases the ailerons ___

A

up to move the wing’s centre of pressure inwards to reduce wing bending

25
Q

TOCWS will be activated as a result of:

A
  • Control locks not removed
  • Powered flying controls INOP
  • Feel simulators INOP
  • Flap settings incorrect
  • Slat settings incorrect
  • Trim outside of limits
  • Aileron upset armed but not applied
  • Speedbrakes/spoilers not in
  • Doors not locked