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Engineering, 02.11.2019 04:31 chris3633

Consider a low-speed open-circuit wind tunnel operating at sea level with a nozzle contraction ratio of 12. when the tunnel is turned on, the pressure difference betweenthe inlet (the settling chamber) and the test section is read as a height difference of 10 cm on au-tube mercury manometer. (the density of liquid mercury is 1.36 x 104 kg/m3). calculate the velocity of the air in the test section.

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Consider a low-speed open-circuit wind tunnel operating at sea level with a nozzle contraction ratio...

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