NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
On the Implementation and Further Validation of a Time Domain Boundary Element Method Broadband Impedance Boundary ConditionA time domain boundary integral equation with Burton-Miller reformulation is presented for acoustic scattering by surfaces with liners in a uniform mean flow. The Ingard-Myers impedance boundary condition is implemented using a broadband multipole impedance model and converted into time domain differential equations to augment the boundary integral equation. The coupled integral-differential equations are solved numerically by a March-On-in-Time (MOT) scheme. While the Ingard-Myers condition is known to support Kelvin-Helmholtz instability due to its use of a vortex sheet interface between the flow and the liner surface, it is found that by neglecting a second derivative term in the current time domain impedance boundary condition formulation, the instability an be effectively suppressed in
computation. The proposed formulation and implementation are validated using a NASA Langley Research Center Grazing Flow Impedance Tube (GFIT) experimental dataset with satisfactory results. Moreover, a minimization procedure for finding the poles and coefficients of the broadband multiple impedance model is formulated in this paper by which, unlike the commonly used vector-fitting method, passivity of the model is ensured. Numerical tests show the proposed minimization approach is effective for modeling liners that are commonly used in aeroacoustic applications.
Document ID
20220007336
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Fang Q Hu
(Old Dominion University Norfolk, Virginia, United States)
Douglas M Nark
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 11, 2022
Subject Category
Acoustics
Meeting Information
Meeting: 28th AIAA/CEAS Aeroacoustics Conference
Location: Southampton
Country: GB
Start Date: June 14, 2022
End Date: June 17, 2022
Sponsors: Council of European Aerospace Societies, American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 081876.02.07.15.01.03.03
CONTRACT_GRANT: SPEC5732
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Time Domain Impedance Boundary Condition
Acoustic Scattering
Time Domain Boundary Element Method
Burton-Miller reformulation
No Preview Available