Stick-Free Long. St&Cnt (SS&C-8) Flashcards

1
Q

The pressure distribution over the surface of a plane flap is governed by what two parameters?

A
  1. Angle of attack

2. Deflection of the flap (or elevator)

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2
Q

The asymmetric pressure distribution causes the flap to ______.

A

Float up

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3
Q

The floating tendency is due to what derivative?

A

C_h_alpha

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4
Q

As the flap floats upward, the pressure distribution changes along the chord. What stability derivative determines this phenomenon?

A

C_h_delta

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5
Q

C_h_delta provides a _____ force with respect to float.

A

Restorative

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6
Q

C_h_alpha causes a _____ force with respect to float.

A

Divergent

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7
Q

True or False

On most control surfaces, it is important to get the floating tendency as close to zero as possible.

A

True

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8
Q

For the pilot to control the aircraft without undue force, ____ must have a shallow (low) slope, especially for high-speed airplanes.

A

C_h_delta

Perkins and Hage, Pg. 273

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9
Q

Why is lifting line theory not successful in predicting hinge moment effects?

A

Because it doesn’t take into account viscous (boundary layer) phenomena.

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10
Q

True or False

Generally on most control surfaces, it is important to get the floating tendency to as near 0 as possible.

A

True

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11
Q

The slope of ____ must be as close as possible to zero to try and reduce the floating tendency.

A

C_h_alpha

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12
Q

What is the major technique used in aerodynamic balancing?

A

The set-back hinge.

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13
Q

If the setback hinge is placed too far aft with respect to the pressure distribution the control is referred to as ______

A

Overbalanced

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14
Q

What are the three methods for the prediction of hinge moments?

A
  1. Semi-analytical/empirical analysis
  2. Wind tunnel tests
  3. CFD
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15
Q

Why are wind tunnel tests, in order to study hinge moments, often difficult and ineffective?

A

Because dynamic similarity is almost impossible to achieve and requires some form of artificial transitting of the local flow to approximate a solution.

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16
Q

What are the three primary geometric factors that can affect the hinge moment?

A
  1. Nose shape
  2. Nose gap
  3. Hinge axis location
17
Q

What are the three most common design options that can affect the hinge moment?

A
  1. Horn balance
  2. Sealed control surface
  3. Beveled trailing edge
18
Q

What is the benefit of a horn balance?

A

Outer aerodynamic surface moments balance control surface moments.

19
Q

What is the benefit of a sealed control surface?

A

This eliminates air bleed from the lower to the upper surface.

20
Q

What is the benefit of a beveled trailing edge?

A

It controls the aft separation of flow, increasing the effectiveness.

21
Q

What is a trim tab and what is its primary purpose?

A

An ancillary surface attached to the trailing edge of the control surface. It is used to create moments about the control hinge axis to trim or balance the flap.

22
Q

True or False

The trim tab can be used as a primary control device.

A

True

23
Q

True or False

The deflection of the trim tab determines the equilibrium elevator angle.

A

True

24
Q

True or False

The trim tab allows one to set a controlled deflection without a constant input force from the pilot.

A

True