Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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Air enters a rectangular duct at T₁ = 300 K, P₁ = = 420 kPa, and Ma₁ = 2. Heat is transferred to the air in the = amount of 55 kJ/kg as it flows through the duct. Disregarding frictional losses, determine the temperature and Mach number at the duct exit.
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- An aircraft is flying at 440 km/hr at 3 km on a standard day. What is the aircraft Mach Number?arrow_forwardAir flows into a converging duct, and a normal shock stands at the exit of the duct. Downstream of the shock, the Mach number is 0.54. If p2/p1 = 2, compute the Mach number at the entrance of the duct and the area ratio A1/A2.arrow_forward
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