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2. The wing on an aircraft is subjected to a drag F, created by airflow over its surface. It is anticipated that this force i
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Q. Independent parameters for the system are 8 (density) ul Viscosity) el characteristic length) V( Flow relocity) Dependentto = f (P, H, I, V) f(Fo, 2, 4, 6, V) =0 Number of independent parameters involved (m=5) Numbes of basic dimensions innoluedSo, Dimensionless parameters are R, Fo P v² 1 2 R2 = M PV I 2

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