5.35 Subsonic aircraft use a pitot tube (impact pressure tube) and a static pressure port to determine aircraft airspeed by U = 2Ap Pair 2PH₂8H = where H = Aр/Pнg is Pair the differential pressure expressed in either inches Hg or mm Hg. The value of H can be measured to within 1% (95%) uncertainty. For a measured H of 20 mm Hg, estimate the airspeed and the uncertainty in airspeed at sea level due to H. Use International Standard Atmosphere (ISA) conditions of 15°C and 101,320 Pa abs. For the densities, use PH₂(kg/m³) = 13595-2.57(°C) ±0.1 and treat dry air as an ideal gas so that pair (kg/m³) 3.4837 x 10³p(Pa abs)/T(K) ± 0.001. Neglect the uncertainties in the two densities in the analysis. =
5.35 Subsonic aircraft use a pitot tube (impact pressure tube) and a static pressure port to determine aircraft airspeed by U = 2Ap Pair 2PH₂8H = where H = Aр/Pнg is Pair the differential pressure expressed in either inches Hg or mm Hg. The value of H can be measured to within 1% (95%) uncertainty. For a measured H of 20 mm Hg, estimate the airspeed and the uncertainty in airspeed at sea level due to H. Use International Standard Atmosphere (ISA) conditions of 15°C and 101,320 Pa abs. For the densities, use PH₂(kg/m³) = 13595-2.57(°C) ±0.1 and treat dry air as an ideal gas so that pair (kg/m³) 3.4837 x 10³p(Pa abs)/T(K) ± 0.001. Neglect the uncertainties in the two densities in the analysis. =
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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