TY - GEN
T1 - Time-domain calculation of sound propagation in lined ducts with sheared flows
AU - Özyörük, Yusuf
AU - Long, Lyle N.
N1 - Publisher Copyright:
© by Y. Özyörük and L.N. Long. Published by the American Institute of Aeronautics, Inc.
PY - 1999
Y1 - 1999
N2 - A recent application of the time-domain equivalent of the classical acoustic impedance condition, i.e. the particle displacement continuity equation, to the numerical simulations of a flow-impedance tube in the time domain yielded reasonably good results with uniform mean flows. The present paper extends this application to include sheared mean flow effects on sound propagation over acoustically treated walls. To assess the prediction improvements with sheared flows, especially at relatively high Mach numbers, numerical simulations of the NASA Langley flow-impedance tube are carried out at actual conditions. Calculations are realized for mean flow peak velocities as high as Mach 0.5 at various frequencies. Results are compared with those obtained with uniform mean flows and experimental data. It is shown that solutions which were not attainable previously with uniform flows at high Mach numbers can now be obtained without any problems with the use of sheared background flows.
AB - A recent application of the time-domain equivalent of the classical acoustic impedance condition, i.e. the particle displacement continuity equation, to the numerical simulations of a flow-impedance tube in the time domain yielded reasonably good results with uniform mean flows. The present paper extends this application to include sheared mean flow effects on sound propagation over acoustically treated walls. To assess the prediction improvements with sheared flows, especially at relatively high Mach numbers, numerical simulations of the NASA Langley flow-impedance tube are carried out at actual conditions. Calculations are realized for mean flow peak velocities as high as Mach 0.5 at various frequencies. Results are compared with those obtained with uniform mean flows and experimental data. It is shown that solutions which were not attainable previously with uniform flows at high Mach numbers can now be obtained without any problems with the use of sheared background flows.
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M3 - Conference contribution
AN - SCOPUS:84983151006
SN - 9780000000002
T3 - 5th AIAA/CEAS Aeroacoustics Conference and Exhibit
BT - 5th AIAA/CEAS Aeroacoustics Conference and Exhibit
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - Aeroacoustics Conference and Exhibit, AIAA/CEAS 1999
Y2 - 10 May 1999 through 12 May 1999
ER -