1–19 von 19 Ergebnissen
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    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

    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

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

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

    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