Aerospace Engineering > GATE 2015 > Aircraft Instruments
The Pitot tube of an aircraft registers a pressure p0=54051 N/m2 The static pressure, density and the ratio of specific heats of the freestream are p∞=45565 N/m2, ρ∞=0.6417 kg/m3 and γ=1.4 respectively. The indicated airspeed (in m/s) is
Correct : a
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