1–39 von 39 Ergebnissen
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    Acoustic Scattering for Rotational and Translational Symmetric Structures in Nonuniform Potential Flow

    Karimi, M. / Croaker, P. / Peake, N. et al. | AIAA | 2017

      Acoustic Scattering for Rotational and Translational Symmetric Structures in Nonuniform Potential Flow

      Karimi, M | Online Contents | 2017
      Beteiligte: Peake, N , Kessissoglou, N

    Approximate method for the prediction of propeller noise near-field effects

    PEAKE, N. / BOYD, W. K. | AIAA | 1993

    The noise downstream of a cascade of loaded airfoils

    Peake, N. / Kerschen, E. | AIAA | 2001

    Prediction of acoustic resonance in tandem cascades

    Woodley, B. / Peake, N. | AIAA | 1998

    Automatische Steuerung von passiven, gezogenen Geräten

    Freier Zugriff
    STRONGER BRAD A / ARAL GURCAN / PEAKE JOHN W | Europäisches Patentamt | 2017

    Acoustic radiation from a scarfed cylinder

    Keith, G. / Peake, N. | AIAA | 1998

    Vortex shedding from a cascade of aerofoils

    Woodley, B. / Peake, N. | AIAA | 1997

    The Unsteady Flow Past a Supersonic Splitter Plate

    Peake, N. / Crighton, D. G. / AIAA | British Library Conference Proceedings | 1993

    Tunnelling effects for acoustic waves in slowly varying axisymmetric flow ducts

    Nielsen, R.B | Online Contents | 2016
    Beteiligte: Peake, N

      Tunnelling effects for acoustic waves in slowly varying axisymmetric flow ducts

      Nielsen, R.B | Online Contents | 2016
      Beteiligte: Peake, N

    Bio-Inspired Trailing Edge Noise Control

    Clark, Ian / Alexander, William N. / Devenport, William J. et al. | AIAA | 2015

    Experimental and Theoretical Analysis of Bio-Inspired Trailing Edge Noise Control Devices

    Clark, Ian / Baker, David / Alexander, William N. et al. | AIAA | 2016

    Modal Scattering at an Impedance Transition in a Lined Flow Duct AIAA Paper 2005-2852

    Rienstra, S. / Peake, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005

    The importance of the unsteady Kutta condition when modelling gust–aerofoil interaction

    Ayton, Lorna J | Online Contents | 2016
    Beteiligte: Peake, N

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

    Morsbøl, J.O | Online Contents | 2016
    Beteiligte: Peake, N

    Transient growth and rotor–stator interaction noise in mean swirling duct flow

    Cooper, A.J. | Online Contents | 2006
    Beteiligte: Peake, N.

    The Application of Air-Jet Vortex Generators to Control the Flow on Helicopter Rotor Blades

    Lewington, N. P. / Peake, D. J. / Henry, F. S. et al. | British Library Conference Proceedings | 2000

    HIGH-WAVENUMBER ACOUSTIC RADIATION FROM A THIN-WALLED AXISYMMETRIC CYLINDER

    Keith, G.M. | Online Contents | 2002
    Beteiligte: Peake, N.

    HIGH-WAVENUMBER ACOUSTIC RADIATION FROM A THIN-WALLED SCARFED CYLINDER

    Keith, G.M. | Online Contents | 2002
    Beteiligte: Peake, N.

    VIBRATIONS OF SANDWICH PLATES WITH CONCENTRATED MASSES AND SPRING-LIKE INCLUSIONS

    Sorokin, S.V. | Online Contents | 2000
    Beteiligte: Peake, N.

    Acoustic Resonance in Aeroengine Intake Ducts

    Cooper, A.J. | Online Contents | 2004
    Beteiligte: Peake, N.

    Parametric Study of an Air-Jet Vortex Generator Configuration to Control Rotorcraft Retreating Blade Stall

    Singh, C. / Peake, D. J. / Kokkalis, A. et al. | British Library Conference Proceedings | 2005