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WingCalculations

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drag_coeff_0.m

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4 lines (4 loc) · 101 Bytes

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WingCalculations

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drag_coeff_0.m

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4 lines (4 loc) · 101 Bytes

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function out = drag_coeff_0(C_f, FF, S_wet, S_ref)

C_D_0 = C_f * FF * S_wet / S_ref;

out = C_D_0;

end

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