Axial flow compressors are key components in gas turbines and jet engines, designed to increase the pressure of incoming air through successive stages of rotating and stationary blades. The rotating blades, known as rotors, accelerate the airflow, while the stationary blades, or stators, convert this kinetic energy into pressure. Each stage in the compressor progressively raises the air pressure, ensuring efficient combustion in the engine. The streamlined design of these components minimizes energy losses and enhances overall performance.