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A mathematical model for simulating noise suppression of lined ejectorsA mathematical model containing the essential features embodied in the noise suppression of lined ejectors is presented. Although some simplification of the physics is necessary to render the model mathematically tractable, the current model is the most versatile and technologically advanced at the current time. A system of linearized equations and the boundary conditions governing the sound field are derived starting from the equations of fluid dynamics. A nonreflecting boundary condition is developed. In view of the complex nature of the equations, a parametric study requires the use of numerical techniques and modern computers. A finite element algorithm that solves the differential equations coupled with the boundary condition is then introduced. The numerical method results in a matrix equation with several hundred thousand degrees of freedom that is solved efficiently on a supercomputer. The model is validated by comparing results either with exact solutions or with approximate solutions from other works. In each case, excellent correlations are obtained. The usefulness of the model as an optimization tool and the importance of variable impedance liners as a mechanism for achieving broadband suppression within a lined ejector are demonstrated.
Document ID
19940028424
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Watson, Willie R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1994
Subject Category
Acoustics
Report/Patent Number
NASA-TP-3425
NAS 1.60:3425
L-17283
Report Number: NASA-TP-3425
Report Number: NAS 1.60:3425
Report Number: L-17283
Accession Number
94N32930
Funding Number(s)
PROJECT: RTOP 505-59-52-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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