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NASA NTRS · 19760050025

Cylindrical diffuser performance using a truncated plug nozzle

Abstract

Cylindrical diffuser performance for a truncated plug nozzle without external flow was tested in a blowdown wind tunnel. The nozzle was designed for an exit Mach number of 1.9 and the plug was conical in shape from the throat and converged to the axis of symmetry at an angle of 10 degrees. The diffuser section was fashioned into two 13.97 cm lengths to facilitate boring of the duct diameter and to allow for testing of two different duct lengths. A slotted hypotube was installed in the base of the diffuser to measure pressure distribution down the centerline of the diffuser. The data obtained included: the typical centerline and sidewall pressure ratio variation along the diffuser, cell pressure ratio vs overall pressure ratio for long and short diffusers and a comparison of minimum experimental cell pressure ratio vs area ratio.

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BibTeXRIS

Galanga, F. L., Mueller, T. J.. 1976-04-01. Cylindrical diffuser performance using a truncated plug nozzle. https://ntrs.nasa.gov/citations/19760050025

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