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    A New Algorithm for Shock Sensor Calculation at Supersonic Speeds on a 3D-Unstructured Grid by Vahid Tahmasbi, Seyed Mohammad Hossein Karimian

    Published 2016-10-01
    “…The new algorithm, implemented at an in-house code, is evaluated by comparison of its results with wind tunnel test data and upwindtype differencing scheme of Roe for a tailplane model tested at Royal Aircraft Establishment. The results show that supersonic flow with shock waves has been accurately captured.…”
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  3. 3

    Robust control system design with application to high performance helicopters by Tombs, M

    Published 1987
    “…The system considered was an unstable helicopter model, obtained from a large nonlinear simulation (provided by the Royal Aircraft Establishment, Bedford) configured to represent future high performance helicopters. …”
    Thesis