![4.37 As shown in Fig. P4.37, air enters the diffuser of a jet engine operating at steady state at 18 - YouTube 4.37 As shown in Fig. P4.37, air enters the diffuser of a jet engine operating at steady state at 18 - YouTube](https://i.ytimg.com/vi/WbX2neeBBDE/maxresdefault.jpg)
4.37 As shown in Fig. P4.37, air enters the diffuser of a jet engine operating at steady state at 18 - YouTube
![As shown, air enters the diffuser of a jet engine at 18 kPa, 216 K with a velocity of 265 m/s, all data corresponding to high altitude flight. The air flows adiabatically As shown, air enters the diffuser of a jet engine at 18 kPa, 216 K with a velocity of 265 m/s, all data corresponding to high altitude flight. The air flows adiabatically](https://homework.study.com/cimages/multimages/16/03.26.82310504632637253129.jpg)
As shown, air enters the diffuser of a jet engine at 18 kPa, 216 K with a velocity of 265 m/s, all data corresponding to high altitude flight. The air flows adiabatically
![Five Axis Machining Aluminum Diffuser Parts for Turbojet Engine - China Turbine Engine, Die Casting | Made-in-China.com Five Axis Machining Aluminum Diffuser Parts for Turbojet Engine - China Turbine Engine, Die Casting | Made-in-China.com](https://image.made-in-china.com/2f0j00bdVhpiUWZCgB/Five-Axis-Machining-Aluminum-Diffuser-Parts-for-Turbojet-Engine.webp)
Five Axis Machining Aluminum Diffuser Parts for Turbojet Engine - China Turbine Engine, Die Casting | Made-in-China.com
![A turbojet engine operates at the following state values: Inlet to the diffuser: 30 kPa, 220 K, 200 m/s Mass flow rate: 20 kg/s Compressor pressure ratio: 10 Combustor exit temperature: 1500 A turbojet engine operates at the following state values: Inlet to the diffuser: 30 kPa, 220 K, 200 m/s Mass flow rate: 20 kg/s Compressor pressure ratio: 10 Combustor exit temperature: 1500](https://homework.study.com/cimages/multimages/16/turbojet-13811184051767746306.jpg)