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Visualization of fan chevron nozzle

Propulsion Airframe Aeroacoustic Computational Analysis

The complex interaction of an asymmetrical fan chevron nozzle with the asymmetrical effect of a jet-pylon interaction as visualized by the computation of turbulent kinetic energy.

Credit: Research by Khaled Abdol-Hamid, S. Paul Pao, Russ Thomas, Craig Hunter, NASA Langley Research Center; Steven Massey, Eagle Aeronautics, Inc.; Alaa Elmilligui, Analytical Services & Materials, Inc.

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