1 Introduction Flashcards

1
Q

What is dynamic aeroelasticity?

A

Dynamic Aeroelasticity is the oscillatory effects of the interaction between aerodynamic, inertia and elastic forces for a flexible structure.
(Pic 1)

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2
Q

What is static aeroelasticity?

A

The nonoscillatory effects of aerodynamic forces interacting with elastic forces in the flexible aircraft structure.

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3
Q

What are some negatives if STATIC aeroelasticity is too high?

A
  • Potential reduction in control effectiveness and possible control reversal.
  • Potential divergence (e.g. twist increases without limit)
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4
Q

What are some negatives if DYNAMIC aeroelasticity is too high?

A

Flutter the unfavourable coupling between two or more vibration modes leading to potential instability (extraction of energy from
airstream)

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5
Q

What is the centre of pressure?

A

The point that the aerodynamic forces act around.

It moves as the angle changes

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6
Q

3D Lift equation

A
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7
Q

2D Lift Equation

A

Where c is the cord length

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8
Q

2D Drag Equation

A

Where c is the chord length

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9
Q

3D Drag Equation

A
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10
Q

3D Pitching Moment Equation

A

extra *c, compared to the other

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11
Q

2D Pitching Moment Equation

A
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12
Q

Reynolds number equation

A

u = velocity
D = characteristic length

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13
Q

Air Density Equation

A
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14
Q

How does pitching moment coefficient at the aerodynamic centre change with incidence or CL?

A

Cmx=Cm0
Pitching moment coefficient does not change with angle.

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15
Q

What is the 2D CL graph equation?

A
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16
Q

What is a1?

A

The gradient of the 2D CL curve

17
Q

What is a0?

A

Zero lift angle of attack

18
Q

What is

A

It is the moment coefficient at the zero lift condition.

19
Q

What is the lift on a strip (dL) equation?

A
20
Q

What is aw?

A

The 3D coefficient lift curve slope

21
Q

When is the coefficient of moments = to zero?

A

At the aerodynamic centre (ac)

22
Q

What is the Total Lift from the strip theory?

A

Acts at quarter chord

23
Q

What’s the relationship between moment and lift coefficients below stall?

A
24
Q

Equation to get the CM at a random place:

A
25
Q

What is the density at sea level?

A

1.225 kg/m^3

26
Q

How to go from true equivalent air speed to true airspeed?

A
27
Q

What does q derive for in most places for this module?

A

The dynamic pressure

28
Q

What is special about the centre of pressure?

A

No matter what, the pitching moment coefficient doesn’t change.