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NASA NTRS · 19870058569

Compressible flow in a diffusing S-duct with flow separation

Abstract

Local flow velocity vectors, as well as static and total pressures along ten radial traverses, were obtained at six stations for secondary flows in a diffusing 30-30-deg S-duct with circular cross section. The strong secondary flow measured in the first bend continued into the second with new vorticity produced in the opposite direction. Contour plots representing the transverse velocity field, as well as total and static pressure contours, have been obtained. As a result of the secondary flow and subsequent separation, substantial total pressure distortion is noted to occur at the duct exit.

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Vakili, A. D., Wu, J. M., Bhat, M. K., Liver, P.. 1987-01-01. Compressible flow in a diffusing S-duct with flow separation. https://ntrs.nasa.gov/citations/19870058569

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