combustion chamber consists of combustion pipes with a diameter of 15 cm. Compressed air enters the pipes at 550 K, 480 kPa and 80 m / s (Figure 3). Calorific value (ID) A fuel of 42000 kJ / kg will be into air, the mass air-fuel ratio (HY) will be 40. injected and burned. A heat transfer to the air thinking like, at the exit of the combustion chamber a) Temperature, b) Pressure, c) Find the speed and Mach number values. k=1.4, cp=1.005 kJ/kg.K, R=0.287 kJ/kg.K
combustion chamber consists of combustion pipes with a diameter of 15 cm. Compressed air enters the pipes at 550 K, 480 kPa and 80 m / s (Figure 3). Calorific value (ID) A fuel of 42000 kJ / kg will be into air, the mass air-fuel ratio (HY) will be 40. injected and burned. A heat transfer to the air thinking like, at the exit of the combustion chamber a) Temperature, b) Pressure, c) Find the speed and Mach number values. k=1.4, cp=1.005 kJ/kg.K, R=0.287 kJ/kg.K
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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A combustion chamber consists of combustion pipes with a diameter of 15 cm. Compressed air enters the pipes at 550 K, 480 kPa and 80 m / s (Figure 3). Calorific value (ID) A fuel of 42000 kJ / kg will be into air, the mass air-fuel ratio (HY) will be 40. injected and burned. A heat transfer to the air thinking like, at the exit of the combustion chamber a) Temperature, b) Pressure, c) Find the speed and Mach number values.
k=1.4, cp=1.005 kJ/kg.K, R=0.287 kJ/kg.K
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