NACABladeMOI:
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Approximates the mass moment of inertia about a point on the blade
cross-section for symmetrical NACA blades.
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Form:
MOI = NACABladeMOI(d)
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Inputs
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d (1,1) Data structure
.t (1,1) Thickness Ratio
.c (1,1) Chord length (m)
.x0 (1,1) X Coordinate of Rotation Axis (m)
.y0 (1,1) Y Coordinate of Rotation Axis (m)
.M (1,1) Mass (kg)
.dx (1,1) Resolution (m)
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Outputs
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MOI (1,1) Moment of Inertia (kg*m^2)
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Reference:
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