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Turbulence Measurements of Rectangular Nozzles with BevelThis paper covers particle image velocimetry measurements of a family of rectangular nozzles with aspect ratios 2, 4, and 8, in the high subsonic flow regime. Far-field acoustic results, presented previously, showed that increasing aspect ratios increased the high frequency noise, especially directed in the polar plane containing the minor axis of the nozzle. The measurements presented here have important implications in the modeling of turbulent sources for acoustic analogy theories. While the nonaxisymmetric mean flow from the rectangular nozzles can be studied reliably using computational solutions, the nonaxisymmetry of the turbulent fluctuations, particularly at the level of velocity components, cannot; only measurements such as these can determine the impact of nozzle geometry on acoustic source anisotropy. Additional nozzles were constructed that extended the wide lip on one side of these nozzles to form beveled nozzles. The paper first documents the velocity fields, mean and variance, from the round, rectangular, and beveled rectangular nozzles at high subsonic speeds. A second section introduces measures of the isotropy of the turbulence, such as component ratios and lengthscales, first by showing them for a round jet and then for the rectangular nozzles. From these measures the source models of acoustic analogy codes can be judged or modified to account for these anisotropies.
Document ID
20150002851
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Bridges, James
(NASA Glenn Research Center Cleveland, OH United States)
Wernet, Mark P.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
March 13, 2015
Publication Date
January 5, 2015
Subject Category
Aircraft Propulsion And Power
Acoustics
Report/Patent Number
GRC-E-DAA-TN19489
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition 2015
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 475122.02.03.05.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Rectangular Nozzle
Jet Flow
Turbulence
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