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      Designing a Facility for Measuring Higher-Order Acoustic Modes in Uniform Heated Flows

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          Abstract

          An experimental facility was recently developed at the Georgia Tech Research Institute to measure the acoustic scattering coefficients of a test article under mean flow, high-temperature, high-amplitude, and higher-order mode propagation conditions. The experimental facility acts like a two-sided impedance tube, in which the measurement section is a circular duct with 16 acoustic drivers and 16 microphones mounted on each side of the test article. Such a facility can be configured for grazing and bias flow measurements of acoustic liners with sound traveling in and against the direction of the flow. The new facility is designed to maximize the accuracy of acoustic measurements of higher-order modes in heated flows. The influence of experimental uncertainties on the acoustic measurements is analyzed using a Monte Carlo method. Measurements of half-wave resonators in quiescent air and heated flows demonstrate that the experimental uncertainty decreases as the absorption coefficient increases. High-sensitivity microphones produce extremely low uncertainty, and even lower-sensitivity pressure transducers are sufficiently accurate for many applications. This paper is intended to serve as a reference for designing and analyzing an experimental facility to measure the acoustic scattering coefficients in heated-flow and higher-order mode propagation conditions.

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          Most cited references39

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          Transfer function method of measuring in‐duct acoustic properties. I. Theory

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            Acoustics of Aircraft Engine-Duct Systems

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              Error analysis of two‐microphone measurements in ducts with flow

                Author and article information

                Contributors
                Conference
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                10 December 2021
                April 2022
                : 60
                : 4
                : 2354-2366
                Affiliations
                Georgia Institute of Technology and Georgia Tech Research Institute , Atlanta, Georgia 30332
                Author notes
                [*]

                Ph.D. Student, Daniel Guggenheim School of Aerospace Engineering; currently at Blue Ridge Research and Consulting, LLC. Member AIAA.

                [†]

                Research Engineer. Member AIAA.

                [‡]

                Undergraduate Student, Daniel Guggenheim School of Aerospace Engineering; currently at Northrop Grumman Corporation. Member AIAA.

                [§]

                Principal Research Engineer. Associate Fellow AIAA.

                [¶]

                Regents Professor, Daniel Guggenheim School of Aerospace Engineering & Regents Researcher and Chief, Aerospace and Acoustics Technologies Division, Aerospace, Transportation, and Advanced Systems Laboratory. Fellow AIAA.

                Article
                J060844 J060844
                10.2514/1.J060844
                e4d5ca59-95b3-41c6-b4a3-3cedd83a0eaf
                Copyright © 2021 by Shane V. Lympany, Aharon Z. Karon, Madison L. Wadsworth, Robert Funk, and Krishan K. Ahuja. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 24 April 2021
                : 13 September 2021
                : 20 October 2021
                Page count
                Figures: 14, Tables: 3
                Funding
                Funded by: National Science Foundation Graduate Research Fellowship Program
                Award ID: DGE-1650044
                Categories
                Regular Articles
                p2291, Thermophysics and Heat Transfer
                p16692, Heat Transfer
                p4070, Thermocouples
                p3973, Combustion Chambers
                p3350, Heat Exchangers
                p2071, Thermodynamic Properties
                p27824, Mass Transfer
                c41, Phase Transition
                p2263, Fluid Dynamics
                p3997, Monte Carlo Method

                Engineering,Physics,Mechanical engineering,Space Physics
                Data Acquisition System,Heat Flow,Monte Carlo Simulation,Acoustic Scattering,Flow Measurement,Static Pressure,Mach Number,Absorption Coefficient,Pressure Transducers,Acoustic Measurement

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