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Engineering, 07.12.2019 05:31 moldybubblegum11

Apitot tube, mounted on an airplane flying at 8000 m standard altitude, reads a stagnation pressure of 58.2 kpa. estimate (a) the velocity in mi/h and (b) the mach num

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Apitot tube, mounted on an airplane flying at 8000 m standard altitude, reads a stagnation pressure...
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