NASA NTRS ยท 19820014584
Turbofan forced mixer-nozzle internal flowfield. Volume 1: A benchmark experimental study
Abstract
An experimental investigation of the flow field within a model turbofan forced mixer nozzle is described. Velocity and thermodynamic state variable data for use in assessing the accuracy and assisting the further development of computational procedures for predicting the flow field within mixer nozzles are provided. Velocity and temperature data suggested that the nozzle mixing process was dominated by circulations (secondary flows) of a length scale on the order the lobe dimensions which were associated with strong radial velocities observed near the lobe exit plane. The 'benchmark' model mixer experiment conducted for code assessment purposes is discussed.
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Paterson, R. W.. 1982-04-01. Turbofan forced mixer-nozzle internal flowfield. Volume 1: A benchmark experimental study. https://ntrs.nasa.gov/citations/19820014584
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