11.1 Flashcards

1
Q

Which form of drag is reduced by boundary layer control?

A

Reduced Drag

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2
Q

Which of the statements is true? (spoiler and speed brakes)

A

Spoiler and speed brakes always reduce lift and increase drag.

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3
Q

How are leading edge devices deployed?

A

By the same lever as for flap deployment.

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4
Q

Reguarding aerodynamic heating which material looses 80% of its strength at 250 degrees c?

A

Aluminium alloys

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5
Q

What can be said about changes in velocity, pressure and density in a shock wave?

A

Changes occur suddenly and sharply

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6
Q

What happens to the airflow as an aircraft approaches the speed of sound?

A

Areas of supersonic airflow increase and shockwaves move closer to the TE.

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7
Q

What is the increase in lift provided by the slat system?

A

35%

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8
Q

When does the boundary layer loose control with the surface?

A

When kinetic energy in the boundary layer is too low

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9
Q

What is the critical mach?

A

The point at which the local airflow reaches mach 1

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10
Q

When is a control surface correctly balanced?

A

When the centre of gravity is located at the hinge line

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11
Q

What is done to prevent extreme pressures and temps at the engine compressor during high speed flight?

A

One normal, three oblique shockwaves are formed to slow the airflow

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12
Q

What is the disadvantage of an anti balance trim tab?

A

The pilot requires more effort to deflect the control surface

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13
Q

Which tab uses a lever?

A

Control tab type

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14
Q

How is the profile thickness expressed in aerodynamics?

A

As a relationship between actual thickness divided by chord length.

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