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NASA NTRS · 19930061149

Navier-Stokes analysis of three-dimensional S-ducts

Abstract

Full 3D Navier-Stokes computational results are presented for compressible flows within nondiffusing and diffusing S-ducts. The present study provides an understanding of the performance characteristics of typical S-ducts with attached and separated flows and provides a frame of reference for future computational fluid dynamic studies of internal flows with strong secondary flows. The predicted results, which were obtained using both H- and O-grids, are compared with the experimental wall pressures, static and total pressure fields, and velocity vectors. In addition, computed boundary-layer thickness, velocity profiles in wall coordinates and skin friction values are presented. The inviscid contributions to the secondary flows are quantified. The S-duct entrance Mach number was 0.6, and the Reynolds number was 1.76 x 10 exp 6 based on the upstream duct diameter.

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BibTeXRIS

Harloff, G. J., Smith, C. F., Bruns, J. E., Debonis, J. R.. 1993-08-01. Navier-Stokes analysis of three-dimensional S-ducts. https://ntrs.nasa.gov/citations/19930061149

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