Equations chapter 4 Flashcards

1
Q

Primary definitions (lift and pitching moment coefficient)

A

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2
Q

primary definitions (center of pressure)

A

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3
Q

Primary definitions (aerodynamic center)

A

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4
Q

thin airfoil theory (flow-tangency condition) (basic equation and elaborate equation)

A

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5
Q

Thin airfoil theory (kutta condition)

A

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6
Q

Thin airfoil theory (Pressure difference)

A

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7
Q

Thin airfoil theory lift and moment

A

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8
Q

design condition of an airfoil

A

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9
Q

flat plate w_induced (velocity induced by a vortex

A

\frac{\gamma}{2\pir}

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