Single-wire swirl flow turbulence measurements

Abstract

A six-orientation, single wire hot wire technique is used to investigate nonswirling and swirling nonreacting flow in an axisymmetric test section with expansion ratio (test section/inlet nozzle diameter) = 2, which may be equipped with a strong contraction nozzle of area ratio 4 at a contraction nozzle downstream distance/test section diameter value = 2. The flowfield contains corner and central recirculation zones typical of gas turbine and ramjet combustion chambers. Swirl may be imparted to the incoming flow by means of a variable angle vane swirler. The effect of swirl on time mean velocities and complete Reynolds stress tensor is investigated, and extensive results are given for swirl vane angles of zero (swirler removed), 38, 45, 60 and 70 deg. The data are being used to aid in the evolution of turbulence models for these complex flow situations. A directional sensitivity analysis is included, which determines the relative accuracy of the measurement technique to approach velocity orientation.