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
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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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

Q.
P1= 480 kPa
T1= 550 K
P2. T2. V2
Yakma
borusu
V1= 80 m/s
Transcribed Image Text:Q. P1= 480 kPa T1= 550 K P2. T2. V2 Yakma borusu V1= 80 m/s
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