Browsing by Author "Peake, Nigel"

Now showing items 1-18 of 18

  • A WKB approximation of elastic waves travelling on a shell of revolution 

    Morsbøl, JO; Sorokin, SV; Peake, Nigel (ElsevierJournal of Sound and Vibration, 2016-08-04)
    This paper is concerned with the elastic waveguide properties of an infinite pipe with circular cross section whose radius varies slowly along its length. The equations governing the elastodynamics of such shells are derived ...

  • An analytically-based method for predicting the noise generated by the interaction between turbulence and a serrated leading edge 

    Mathews, JR; Peake, Nigel (ElsevierJournal of Sound and Vibration, 2018-05-26)
    This paper considers the interaction of turbulence with a serrated leading edge. We investigate the noise produced by an aerofoil moving through a turbulent perturbation to uniform flow by considering the scattered pressure ...

  • Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows 

    Ayton, Lorna Jane (University of CambridgeDepartment of Applied Mathematics and Theoretical PhysicsChurchill College, 2014-10-07)
    This thesis considers the sound generated by unsteady perturbations interacting with solid aerofoils in background steady flows, in an attempt to further develop analytic models for the noise generated by blades within ...

  • Bio-inspired canopies for the reduction of roughness noise 

    Clark, IA; Daly, CA; Devenport, W; Alexander, WN; Peake, Nigel; Jaworski, JW; Glegg, S (ElsevierJournal of Sound and Vibration, 2016-12-22)
    This work takes inspiration from the structure of the down covering the flight feathers of larger species of owls, which contributes to their ability to fly almost silently at frequencies above 1.6 kHz. Microscope photographs ...

  • Bioinspired trailing-edge noise control 

    Clark, IA; Alexander, WN; Devenport, W; Glegg, S; Jaworski, JW; Daly, C; Peake, Nigel (American Institute of Aeronautics and AstronauticsAIAA Journal, 2017-01-01)
    Strategies for trailing edge noise control have been inspired by the downy canopy that covers the surface of exposed flight feathers of many owl species. Previous wind tunnel measurements demonstrate that canopies of similar ...

  • Interaction of turbulence with the leading-edge stagnation point of a thin aerofoil 

    Ayton, Lorna Jane; Peake, Nigel (Cambridge University PressJournal of Fluid Mechanics, 2016)
    An asymptotic model is constructed to analyse the interaction of turbulence generated far upstream with a thin elliptic-nosed solid body in uniform flow. The leading-edge stagnation point causes significant deformation of ...

  • Noise generation by turbulence-propeller interaction in asymmetric flow 

    Robison, Rosalyn AV; Peake, Nigel (Cambridge University PressJournal of Fluid Mechanics, 2014)
    This paper is concerned with a particular source of both broadband and tonal aeroengine noise, termed Unsteady Distortion Noise (UDN). UDN arises from the interaction between turbulent eddies, which occur naturally in the ...

  • Nonlinear and non-modal stability of structures evolving in shear flows 

    Daly, Conor Anthony (University of CambridgeDepartment of Applied Mathematics and Theoretical Physics, 2014-04-08)
    This thesis explores a range of stability techniques applied to fluid structures that develop in various constant density flows. In particular, the stability of nonlinear structures which develop in rotating plane Couette ...

  • On High-Frequency Sound Generated by Gust-Aerofoil Interaction in Shear Flow 

    Ayton, Lorna Jane; Peake, Nigel (CUPJournal of Fluid Mechanics, 2015-02-04)
    A theoretical model is constructed to predict the far-field sound generated by high-frequency gust–aerofoil interaction in steady parallel shear flow, including the effects of aerofoil thickness. Our approach is to use ...

  • Secondary instability and tertiary states in rotating plane Couette flow 

    Daly, CA; Schneider, Tobias M; Schlatter, Philipp; Peake, Nigel (Cambridge University PressJournal of Fluid Mechanics, 2014-11-14)
    Recent experimental studies have shown rich transition behaviour in rotating plane Couette ow (RPCF). In this paper we study the transition in supercritical RPCF theoretically by determination of equilibrium and periodic ...

  • Spectral study of the Laplace-Beltrami operator arising in the problem of acoustic wave scattering by a quarter-plane 

    Assier, RC; Poon, C; Peake, Nigel (Oxford University PressQuarterly Journal of Mechanics and Applied Mathematics, 2016)
    The Laplace-Beltrami operator on a sphere with a cut arises when considering the problem of wave scattering by a quarter-plane. Recent methods developed for sound-soft (Dirichlet) and sound-hard (Neumann) quarter-planes ...

  • Stability analysis for n -periodic arrays of fluid systems 

    Schmid, PJ; De Pando, MF; Peake, Nigel (Physical Review Fluids, 2017-11-01)
    © 2017 American Physical Society. A computational framework is proposed for the linear modal and nonmodal analysis of fluid systems consisting of a periodic array of n identical units. A formulation in either time or ...

  • The acoustic Green's function for swirling flow in a lined duct 

    Mathews, JR; Peake, Nigel (ElsevierJournal of Sound and Vibration, 2017-05-12)
    This paper considers the acoustic field inside an annular duct carrying mean axial and swirling flow and with either acoustically hard or lined walls. The particular aim is to compute the Green's function, which is required ...

  • The acoustic Green's function for swirling flow with variable entropy in a lined duct 

    Mathews, James; Peake, Nigel
    This paper extends previous work by the authors (Journal of Sound and Vibration, 395:294-316,2017) on the acoustic field inside an annular duct with acoustic lining carrying mean axial and swirling flow so as to allow for ...

  • The acoustics of curved and lined cylindrical ducts with mean flow 

    Brambley, Edward James (University of CambridgeDepartment of Applied Mathematics and Theoretical PhysicsPembroke College, 2007-10-23)
    This thesis considers linear perturbations to the steady flow of a compressible inviscid perfect gas along a cylindrical or annular duct. Particular consideration is given to the model of the duct boundary, and to the ...

  • The Importance of the Unsteady Kutta Condition when Modelling Gust-Aerofoil Interaction 

    Ayton, Lorna Jane; Gill, JR; Peake, Nigel (ElsevierJournal of Sound and Vibration, 2016-06-01)
    The Kutta condition is applied to aerofoils with sharp trailing edges to allow for viscous effects to be considered within a simplified system of equations that are inviscid. This paper discusses in detail the inclusion ...

  • Tunnelling effects for acoustic waves in slowly varying axisymmetric flow ducts 

    Nielsen, RB; Peake, Nigel (ElsevierJournal of Sound and Vibration, 2016-06-22)
    The multiple-scales Wentzel–Kramers–Brillouin (WKB) approximation is used to model the propagation of acoustic waves in an axisymmetric duct with a constriction in the presence of mean flow. An analysis of the reflection ...

  • Turbulence ingestion noise of open rotors 

    Robison, Rosalyn Aruna Venner (University of CambridgeDepartment of Applied Mathematics and Theoretical Physics, 2012-04-10)
    Renewed interest in open rotor aeroengines, due to their fuel efficiency, has driven renewed interest in all aspects of the noise they generate. Noise due to the ingestion of distorted atmospheric turbulence, known as ...