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Topic: Science
Number of pages / Number of words: 3 / 574
Essay's paper body

Any increase

beyond CLMAX causes a decrease in coefficient of lift, so we

call CLMAX AOA the most effective angle of attack.

Lift and Stalls

(1.40)

Boundary Layer

Boundary layer is that layer of airflow over a surface that demonstrates local airflow retardation due to viscosity. It is usually no more than 1mm thick at the leading edge of an

airfoil and grows in thickness as it moves aft over the

surface...


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It is usually no more than 1mm thick at the leading edge of an

airfoil and grows in thickness as it moves aft over the

surface.

Lift and Stalls

(1.41)

List and Describe the Types

of Boundary Layer Airflow

LAMINAR FLOW

In laminar flow, the air molecules move smoothly along in streamlines. The laminar layer produces very little friction, but is easily separated from the surface...


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