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Engineering, 22.02.2020 04:30 huntbuck14
Consider a Pitot static tube mounted on the nose of an experimental airplane. A Pitot tube measures the total pressure at the tip of the probe (hence sometimes called the Pitot pressure), and a Pitot static tube combines this with a simultaneous measurement of the free-stream static pressure. The Pitot and free-stream static measurements are given below for three different flight conditions. Calculate the free-stream Mach number at which the airplane is flying for each of the three different conditions
1. Pitot pressure=1.22×105N/m2 , static pressure=1.01 × 105N/m2 .
2. Pitot pressure=7222lb/f t2 , static pressure=2116lb/f t2 .
3. Pitot pressure=13197lb/f t2 , static pressure=1020lb/f t2 .
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Consider a Pitot static tube mounted on the nose of an experimental airplane. A Pitot tube measures...
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