Abstract
Finding the sound pressure level (SPL) distribution near the ground due to aircraft noise is an important problem in environmental engineering. Since the human hearing range is very wide, ranging from 20 Hz to 20 kHz, the determination of the SPL distribution for a given source spectrum is a difficult multiscale problem, and requires the repeated solution, for many different wave numbers, of the Helmholtz equation in the upper half space, while imposing a given impedance boundary condition on the ground. Previously, a simple computational scheme, based on the use of fictitious sources, was proposed for the efficient solution of such problems, for a flat ground with a given constant impedance. In the present study, this scheme is improved and extended in several ways. First, the ground impedance is allowed to vary with location, representing a varying type of ground (soil, water, asphalt, etc.). Second, a mechanism for verification of the method and for error estimation is developed, whereas previously only the boundary condition residual was evaluated. Third, the use of the appropriate Green’s function, associated with a ringlike source, is made precise. Two simplifying assumptions which are maintained are that the ground is flat and that its impedance function is axially symmetric. Numerical experiments are used to demonstrate the performance of the scheme.
| Original language | English |
|---|---|
| Pages (from-to) | 563-582 |
| Number of pages | 20 |
| Journal | International Journal for Multiscale Computational Engineering |
| Volume | 17 |
| Issue number | 6 |
| DOIs | |
| State | Published - 2019 |
Keywords
- Green's function
- Helmholtz equation
- SPL
- acoustic waves
- aircraft noise
- equivalent sources
- fictitious sources
- ground impedance
- multifrequency
- multiscale
All Science Journal Classification (ASJC) codes
- Control and Systems Engineering
- Computational Mechanics
- Computer Networks and Communications