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  • Item
    1.5µm lidar for helicopter blade tip vortex detection
    ( 2009) Valla, M. ; Augere, B. ; Dolfi, A. ; Goular, D. ; Fleury, D.
  • Item
    1/10th scale model tests of a centre-line tiltrotor: Conversion between rotary and fixed wing modes
    ( 2011) Burrage, B.
  • Item
    11'Heloise': the Agusta project to concurrent engineering
    ( 1993) Camerino, P.
  • Item
    11'Will rotor hubs lose their bearings?': a survey of bearingless
    ( 1992) Huber, H.
  • Item
    2D iced airfoils aerodynamic performance measurements and simulations
    ( 2006) Decours, J. ; Pape, A. Le
  • Item
    2D simulation of unsteady phenomena on a rotor
    ( 1978) Renaud, J. ; Coulomb, J.
  • Item
    2D Unsteady Navier-Stokes computations at ONERA for prediction of
    ( 1998) Rouzaud, O. ; Plop, A.
  • Item
    3D Euler methods for multibladed rotors in hover and forward flight
    ( 1993) Pahlke, K. ; Raddatz, J.
  • Item
    3D laminar-turbulent boundary layer calculations on helicopters
    ( 1995) Beaumier, P. ; Houdeville, R.
  • Item
    3D Mock-up CAD
    ( 2000) Noblet, L.
  • Item
    3D sound and hearing protection for helicopter missions
    ( 2010) Blanc, D. ; Arnod, J.L.
  • Item
    50-years Dutch helicopter-ship qualification
    ( 2016) Booij, P. ; Vorst, J. van der
  • Item
    6 Conclusions
    ( 1998)
  • Item
    90 years of helicopter design, development and testing in the netherlands
    ( 2009) Bakker, K.
  • Item
    A "force-free" rotor wake model for advanced research applications
    ( 1997) Soliman, M.M.
  • Item
    A 10 year retrospective and look ahead at the use of sound and visualisations for stakeholder engagement and understanding perceptions of disruptive technologies
    ( 2021) Hiller, D. ; Maldonado, A.L. ; Jurdic, V. ; Harris, H. ; Heggie, C. ; Hermans, P. ; Sharp, C. ; Thomas, A. ; Woodcock, J.
    Originally conceived and developed to inform the design of some of the world’s best arts and culture venues, over the past 10+ years, Arup SoundLab has also been used to create sound demonstrations that simulate and gauge response to environmental sound. Sound demonstrations combine aural and visual simulations to enable clients, designers, major stakeholders and the general public to experience and better understand sound. They provide robust objective information to support decision making and help shape better outcomes for all. SoundLab has been used to inform the design of vertiport infrastructure; to assess annoyance and possible health impacts of novel noise sources; to inform local and international policy on noise; and to provide information on the early prototyping of Advanced Air Mobility (AAM) vehicles. These applications are described in the paper, including a recent pilot study for the European Union Aviation Safety Agency (EASA). The EASA study provided insight into people’s response to AAM noise impacts, indicating that, in general, annoyance from AAM vehicles could be higher than for other transport modes, which may have implications for planning and legislation for AAM noise. As AAM applications broaden, auralisation and visualisation processes are being developed to facilitate understanding of the multi-faceted AAM planning, permitting and design processes. The immersive experience provides information that is valuable to the various parties involved. These include electric aircraft manufacturers to support understanding of evolving designs; policy makers and planning authorities who may have little knowledge or understanding of these novel noise sources; and airspace designers.
  • Item
    A 2-D dynamic stall model based on a Hopf bifurcation
    ( 1993) Truong, V.K.
  • Item
    A better way to analyse and interpret helicopter handling qualities and workload ratings
    ( 2006) Bradley, R. ; Maclaren, W.M.
  • Item
    A boundary integral formulation for the aerodynamic analysis of
    ( 1993) Visingardi, A.
  • Item
    A comparative analysis of processing structures for airborne systems
    ( 1983) Scotti di Uccio, G.A.

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