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.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fcc44f72d-3f26-42d9-921c-cc5e4ab0fed8%2Fd9f3f5da-2a4b-4c06-bed8-75807f3d0f6f%2F5nl7a3y_processed.jpeg&w=3840&q=75)
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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