1.

A passenger plane flies at an altitude of 8 km at a speed of 900 km/h. The speed is measured with the aid of a Pitot-Prandtl tube. Find the pressure difference in the differential manometer. For data relating to the atmosphere see xi 26.10, Table 26.3.

Answer»


ANSWER :`1.65 xx10^4 ` PA = 124 MM HG


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