Small wind tunnels in an undergraduate laboratory have
305-mm square test sections. Measurements show the
boundary layers on the tunnel walls are fully turbulent and
well represented by 1
7-power profiles. At cross section 1 with
freestream speed U1 5 26.1 m/s, data show that δ1 5 12.2
mm; at section 2 , located downstream, δ2 5 16.6 mm.
Evaluate the change in static pressure between sections 1
and 2 . Estimate the distance between the two sections.
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