The cowling of an aircraft engine is the structure’s removable covering, primarily used for drag reduction and increased cooling. During a standard flight, only around 15-30% of total ram airflow colliding with the engine nacelle will actually enter the structure for cooling. As such, the rest of the ram airflow remains outside of the cowling and cannot be optimally used. To improve upon this, the engine cowl will need to be faired in such a way that air may flow across the cowl with low energy loss.
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