An Efficiently Parallelized High-Order Aeroacoustics Solver Using a Characteristic-Based Multi-Block Interface Treatment and Optimized Compact Finite Differencing

This paper presents the development of a fourth-order finite difference computational aeroacoustics solver. The solver works with a structured multi-block grid domain strategy, and it has been parallelized efficiently by using an interface treatment based on the method of characteristics. More impor...

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Bibliographic Details
Main Authors: Bidur Khanal, Alistair Saddington, Kevin Knowles
Format: Article
Language:English
Published: MDPI AG 2017-05-01
Series:Aerospace
Subjects:
Online Access:http://www.mdpi.com/2226-4310/4/2/29