A pitotstatic tube to be used in 2n airplane for on-flight measurement was calibrated on ground by using air of density 1.20 kg/m? . A measurement taken at an altitude of 3000 m where the ambient pressure and density were 70 kPa (abs) and 0.91 ke/m? respectively, indicated a velocity of 200 m/s by using the above ground level calibration. Estimate the true speed of the airplane [Take k = 1.4 and R = 287 (kg K)l. A pitot-static tube to be used in an airplane for on-flight measurement was calibrated on ground by using air of density 1.20 kg/m3. A measurement taken at analtitude of 3000 m where the ambient pressure and density were 70 kPa (abs) and 0.91 kg/m3 respectively, indicated a velocity of 200 m/s by using the aboveground level calibration. Estimate the true speed of the airplane [Take k = 1.4 and R = 287 J/(kg.K)].

Given, Density, ρ=1.20kg/m3Atmospheric density, ρa=0.91kg/m3Indicated velocity, V= 200m/sAtmospheric…

Answered: A pitot-static tube to be used in an…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

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A pitotstatic tube to be used in 2n airplane for on-flight measurement was calibrated on ground by using air of density 1.20 kg/m? . A measurement taken at an altitude of 3000 m where the ambient pressure and density were 70 kPa (abs) and 0.91 ke/m? respectively, indicated a velocity of 200 m/s by using the above ground level calibration. Estimate the true speed of the airplane [Take k = 1.4 and R = 287 (kg K)l.

A pitot-static tube to be used in an airplane for on-flight measurement was calibrated on ground by using air of density 1.20 kg/m3. A measurement taken at an
altitude of 3000 m where the ambient pressure and density were 70 kPa (abs) and 0.91 kg/m3 respectively, indicated a velocity of 200 m/s by using the above
ground level calibration. Estimate the true speed of the airplane [Take k = 1.4 and R = 287 J/(kg.K)].

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