Bernoulli’s Flashcards

1
Q

Total pressure equation

A

Static+dynamic

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2
Q

What is the stagnation region

A

Area of high static pressure in front of any object with airflow

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3
Q

Total air reaction formula

A

Lift+drag

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4
Q

What is lift

A

Flight force that is part of TAR and acts perpendicular to relative airflow

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5
Q

What is drag

A

Flight force that is part of TAR and acts in the same direction as the relative air flow

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6
Q

What is the center of pressure and how does it vary when AofA increases

A

Point where all the lift is said to act through. Moves forward when AofA is increased

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7
Q

Separation point, what happens when AofA increases.

A

Point that airflow leaves the upper surface of a wing. As AofA increases, separation point increases.

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8
Q

Stall point

A

When the separation point reaches the leading edge

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9
Q

What is a stall

A

A large decrease in lift and a large increase in drag at the same time.

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10
Q

What is the boundary layer

A

Layer of air closest to an object’s surface that slows down from free stream velocity to zero at the objects surface.

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11
Q

Laminar BL

A

Smooth layers of air

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12
Q

Turbulent BL

A

Erratic air flow

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13
Q

5 properties of laminar airflow

A

Smooth flow, gradual velocity profile, thinner, less KE, less skin friction

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14
Q

5 properties of turbulent airflow

A

Erratic particle flow, steeper velocity profile, 10x thicker, more KE, delays separation

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