8.2 Aerodynamics Flashcards

1
Q

Where is air incompressible?

A

Air is incompressible in the subsonic region

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2
Q

If no disturbance how do air streamlines flow?

A

Parallel to each other if there is no disturbance.

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3
Q

What happens to streamlines as the diameter gets smaller

A

The streamlines move closer to each other.

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4
Q

What is the continuity equation?

A

V1 A1 = V2 A2

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5
Q

What is constant in airflow?

A

Density is constant

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6
Q

What is a diffuser outlet?

A

Diffuser outlet when the diameter increases and the speed decreases

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7
Q

What is jet outlet?

A

Jet outlet when the diameter decreases and the speed increases.

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8
Q

What is Bernoulli’s principle?

A

The Bernoulli equation states that total pressure is always the sum of static pressure and dynamic pressure, or in short hand notation, P tot. equals p plus q.

The total pressure remains constant.

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9
Q

When a valve is closed what is true about static and dynamic pressure?

A

Static pressure = Total Pressure

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10
Q

How do we measure the static and dynamic pressure when we have a speed.

A

Measure Total pressure at Inlet - Static Pressure at static port.

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11
Q

If speed increases by four times, and density is constant. What will happens to dynamic pressure?

A

The dynamic pressure increases sixteen times

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12
Q

What does IAS stand for?

A

Indicated air speed

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13
Q

What is true about the point of stagnation?

A

Velocity = 0

No dynamic pressure

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14
Q

Where would you find downwash?

A

Trailing -Edge or downwards flow

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15
Q

What is the Magnus Effect?

A

Mechanically induced circulation of an object

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16
Q

What is a profile?

A

Cross-section of a wing

17
Q

What is the rule of vortices?

A

Always form in pairs and rotate counter-clockwise