A Pitot-static probe is used to measure the speed of an aircraft
flying at β=h= 3908 πm. If the differential pressure
reading is 3.5 πππkPa, determine the speed of the
aircraft.
Given that the temperature, pressure, and density at
altitude βh can be calculated as:
π(πΎπππ£ππ)=15.04β0.00649ΓβT(Kelvin)=15.04β0.00649Γh
π(ππ)=101290(π+273.1288.08)5.256P(Pa)=101290(T+273.1288.08)5.256
π(ππ/π3)=π286.9(π+273.1
A Pitot-static probe is used to measure the speed of an aircraft flying at β=h= 3908 𝑚m. If the differential pre
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A Pitot-static probe is used to measure the speed of an aircraft flying at β=h= 3908 𝑚m. If the differential pre
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