Compressed Air Axial Turbine Design for High-Speed Jet Engine Applications

The design and analysis of a compressed air axial turbine for use with high-speed jet engines is the primary objective of this study. To attain the ideal blade geometry for maximal energy extraction from compressed air, the turbine is designed using sophisticated 3D modeling tools. To replicate jet engine conditions, a smaller prototype is created from lightweight materials and tested in a controlled setting. The project assesses important factors such as rotating speed, efficiency, and pressure decrease. The design adapts to different airflows and operating conditions by integrating adjustable blade angles. The experiment demonstrates the importance of axial turbines in generating thrust by transforming compressed air energy into mechanical power.