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    Standford
    Jun-1997 - Sep-2000

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Category > Applied Sciences Posted 07 May 2017 My Price 8.00

A laboratory wind tunnel

A laboratory wind tunnel has a flexible upper wall that can be adjusted to compensate for boundary-layer growth, giving zero pressure gradient along the test section. The wall boundary layers are well represented by the -L-power velocity profile. AO the inlet the tunnel cross section is square, with height Hi and width W,, each equal to 305 mm. With freestream speed t/, = 26.5 m/s, measurements show that 5, =i 12.2 mm and downstream, S6 = 16.6 mm. Calculate the height of the tunnel walls at section © . Determine the equivalent length of flat plate that would produce the inlet boundary layer thickness. Estimate the streamwise distance between sections (j) and © in the tunnel.

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IT KING
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Status NEW Posted 07 May 2017 11:05 AM My Price 8.00

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