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Offset Stream Technology Test-Summary of ResultsStatistical jet noise prediction codes that accurately predict spectral directivity for both cold and hot jets are highly sought both in industry and academia. Their formulation, whether based upon manipulations of the Navier-Stokes equations or upon heuristic arguments, require substantial experimental observation of jet turbulence statistics. Unfortunately, the statistics of most interest involve the space-time correlation of flow quantities, especially velocity. Until the last 10 years, all turbulence statistics were made with single-point probes, such as hotwires or laser Doppler anemometry. Particle image velocimetry (PIV) brought many new insights with its ability to measure velocity fields over large regions of jets simultaneously; however, it could not measure velocity at rates higher than a few fields per second, making it unsuitable for obtaining temporal spectra and correlations. The development of time-resolved PIV, herein called TR-PIV, has removed this limitation, enabling measurement of velocity fields at high resolution in both space and time. In this paper, ground-breaking results from the application of TR-PIV to single-flow hot jets are used to explore the impact of heat on turbulent statistics of interest to jet noise models. First, a brief summary of validation studies is reported, undertaken to show that the new technique produces the same trusted results as hotwire at cold, low-speed jets. Second, velocity spectra from cold and hot jets are compared to see the effect of heat on the spectra. It is seen that heated jets possess 10 percent more turbulence intensity compared to the unheated jets with the same velocity. The spectral shapes, when normalized using Strouhal scaling, are insensitive to temperature if the stream-wise location is normalized relative to the potential core length. Similarly, second order velocity correlations, of interest in modeling of jet noise sources, are also insensitive to temperature as well.
Document ID
20070034837
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Brown, Clifford A.
(NASA Glenn Research Center Cleveland, OH, United States)
Bridges, James E.
(NASA Glenn Research Center Cleveland, OH, United States)
Henderson, Brenda
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2007
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2007-214992
E-16156
AIAA Paper-2007-3664
Report Number: NASA/TM-2007-214992
Report Number: E-16156
Report Number: AIAA Paper-2007-3664
Meeting Information
Meeting: 28th AIAA/CEAS Aeroacoustics Conference
Location: Rome
Country: Italy
Start Date: May 21, 2007
End Date: May 23, 2007
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies
Funding Number(s)
WBS: WBS 984754.02.07.03.17.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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