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}