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    The Unsteady Flow Past a Supersonic Splitter Plate

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

    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 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

    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