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9. An aircraft aircraft is flying at an altitude of hG = 5.2 km. The Pitot tube tip reads p0 = 55539.62 N/m2. Using this
9. An aircraft aircraft is flying at an altitude of hG = 5.2 km. The Pitot tube tip reads p0 = 55539.62 N/m2. Using this information and details from Example 3.7, calculate the aircraft's velocity (V1) in m/s. (6 Points)
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