meed of the flow in the test section.

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A Pitot tube inside a wind tunnel test section reads a pressure of 320150 Pa. A static pressure and total temperature measurement are 45969 Pa and 537.9
K, respectively.
(a) Calculate speed of the flow in the test section.
Transcribed Image Text:A Pitot tube inside a wind tunnel test section reads a pressure of 320150 Pa. A static pressure and total temperature measurement are 45969 Pa and 537.9 K, respectively. (a) Calculate speed of the flow in the test section.
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