Abstract

Reciprocity is a basic property existing in wave phenomena characterized by complex transmission coefficients. Reciprocity in a duct describes the relationship between the direct response at the duct outlet to a source applied at the inlet and the reverse response at the inlet to a source at the outlet. The reciprocity has been adopted to simplify the methodology for predicting the reverse transmission coefficient from the direct coefficient and vice versa. The existing methods, however, cannot predict the complex form of the coefficient because they only consider the reciprocity in the moduli but neglect the reciprocity in the phases. The study on the reciprocity in a duct with a temperature gradient has hardly been seen. The present work derived a reciprocal equation with a time domain method to characterize the reciprocity in a duct with spatially varying temperature. In addition to considering the reciprocity in the moduli of the direct and reverse transmission coefficients, the proposed method invented a correction term to consider the reciprocity in their phases as well. The correction term was developed from the time delay between the incident and the transmitted pulses in the duct solved with the time domain method. The modified reciprocal equation using the correction term was derived and used to predict the reverse transmission coefficient for calculating exhaust noise of an engine connecting to the duct. The result has shown that the proposed time domain method is an effective approach to accurately describe the phase relationship of waves in flow ducts.

Highlights

  • Reciprocity refers to the symmetric wave transmission between two points in space

  • The present paper proposed a time domain method to derive a reciprocal equation characterizing reciprocity of both moduli and phases in a duct without and with a temperature gradient

  • A time domain numerical method was proposed to derive a modified reciprocal equation to predict the complex form of the reverse transmission coefficient for an expansion chamber

Read more

Summary

INTRODUCTION

Scitation.org/journal/adv analyze the acoustic reciprocity for a duct system under flow conditions with temperature gradients. Liu et al. developed a transient CFD approach to fully characterize acoustic responses of a duct system in the presence of engine exhaust flow with spatially varying temperature. 21 and 22 identified the four reflection and transmission coefficients under direct and reverse flow conditions, the application of the time domain method in analyzing acoustic reciprocity has not been published. The present paper proposed a time domain method to derive a reciprocal equation characterizing reciprocity of both moduli and phases in a duct without and with a temperature gradient. A modified reciprocal equation using the correction term was derived to predict the reverse transmission coefficient from the direct transmission coefficient of the duct under a new flow condition with a temperature gradient. The predicted spectrum was compared with the experimental result in verifying the accuracy of the proposed time domain method

Transmission and reflection coefficients
Background on reciprocity in a duct system
CFD methodology for solving time domain responses
CFD model of an expansion chamber without and with a temperature gradient
Derivation of the modified reciprocity equation
Verification of the modified reciprocal equation
Calculation of TM using reciprocity
Results of exhaust noise
CONCLUSIONS
Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.