![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
PW2000 72-763 ENGINE — DIFFUSER CASE AND HIGH PRESSURE TURBINE (HPT) CASE — ONE-TIME EDDY CURRENT INSPECTION FOR CRACKS
![Energies | Free Full-Text | Variable Geometry in Miniature Gas Turbine for Improved Performance and Reduced Environmental Impact Energies | Free Full-Text | Variable Geometry in Miniature Gas Turbine for Improved Performance and Reduced Environmental Impact](https://www.mdpi.com/energies/energies-13-05230/article_deploy/html/images/energies-13-05230-ag.png)