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Journal ArticleDOI

The Ffowcs Williams–Hawkings equation for hydroacoustic analysis of rotating blades. Part 1. The rotpole

Sandro Ianniello
- 25 Jun 2016 - 
- Vol. 797, pp 345-388
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TLDR
In this paper, the Ffowcs Williams-Hawkings equation was used for the analysis of rotating point sources and the deep difference between the acoustic fields generated by aeronautical and marine devices in air and underwater.
Abstract
This paper deals with the use of the Ffowcs Williams–Hawkings equation for hydroacoustic analysis of rotating blades, and the deep difference between the acoustic fields generated by aeronautical and marine devices in air and underwater. This dissimilarity does not depend on either the different fluid or the (although existing) geometric and structural difference of the blade: it is an intrinsic feature of the generating noise mechanisms related to rotating sources and is essentially due to the remarkable diversity of the rotational speed. It will be shown how the usual assumption of believing the flow nonlinear sources to be negligible for blades rotating at low subsonic speed (coming from decades of research strictly limited to aeroacoustics) is totally wrong when applied to hydroacoustics. Such a goal is achieved through a practical approach, by analysing the general behaviour of the surface integral kernels of the solution for a rotating point source (here named rotpole), and by showing its relationship with a general multibladed device. This analysis suggests that the underwater noise prediction from a marine propeller is an inherently nonlinear problem and, contrary to analogous aeronautical configurations, it always requires an accurate estimation of the nonlinear flow sources just by virtue of the very low rotational speed.

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Citations
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Journal ArticleDOI

Characterization of the wake of a submarine propeller via Large-Eddy simulation

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The wake structure of a propeller operating upstream of a hydrofoil

TL;DR: In this paper, large eddy simulations are presented on the wake flow of a notional propeller (the INSEAN E1658), upstream of a NACA0020 hydrofoil of infinite spanwise extent, mimicking propeller-rudder interaction.
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Non-linear noise from a ship propeller in open sea condition

TL;DR: In this paper, the hydrodynamic noise generated by a ship propeller in open sea conditions is investigated. But the authors focus on a single propeller and do not consider the effects of other noise sources.
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The wake flow downstream of a propeller-rudder system

TL;DR: In this article, a largeeddy simulation for the case of a propeller operating upstream of a hydrofoil, mimicking a rudder, is presented, showing that the largest values of turbulent stresses in the wake of a boat are achieved outwards from the radial coordinate of the tip of the propeller blades.
References
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Journal ArticleDOI

Sound Generation by Turbulence and Surfaces in Arbitrary Motion

TL;DR: In this article, sound generation by turbulence and surfaces in arbitrary motion is discussed, and sound and multipole fields and governing equations are discussed. But sound generation is not discussed in this paper.
Journal ArticleDOI

Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces

TL;DR: In this article, the Lighthill acoustic analogy, as embodied in the Ffowcs Williams-Hawkings (FW-H) equation, is compared with the Kirchhoff formulation for moving surfaces.
Journal ArticleDOI

A new boundary integral formulation for the prediction of sound radiation

TL;DR: In this article, a boundary integral formulation is presented for the evaluation of the noise radiated in a uniform medium by generic sources, which is referred as the Kirchhoff-FWH method.
Journal ArticleDOI

Linear Acoustic Formulas for Calculation of Rotating Blade Noise

TL;DR: In this paper, a unified approach is used to derive many of the current formulas for calculation of discrete frequency noise of helicopter rotors and propellers, both compact and non-compact results are derived.
Journal ArticleDOI

Mechanisms of evolution of the propeller wake in the transition and far fields

TL;DR: In this paper, the authors investigated the mechanisms of evolution of propeller tip and hub vortices in the transitional region and the far field of three propellers having the same blade geometry but different number of blades.
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