1–8 von 8 Ergebnissen
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    Helicopter BERP Tip

    Literature Review of Helicopter Blade Shape Optimisation Methods
    Johnson, Catherine S. / Woodgate, Mark / Barakos, George N. | Wiley | 2017
    Schlagwörter: helicopter rotor blade , helicopter BERP tip

    Modelling Helicopter Flight Dynamics: Building a Simulation Model

    Padfield, Gareth D. | Wiley | 2018
    Schlagwörter: helicopter flight dynamics , blade motion

    Active Blade Twist in Rotary UAVs using Smart Actuation

    Marqués, Pascual | Wiley | 2017
    Schlagwörter: helicopter blade , individual blade control , active blade twist technology

    Framework for the Optimisation of a Helicopter Rotor Blade with an Approximate BERP Tip

    Numerical Methods and Application
    Johnson, Catherine S. / Woodgate, Mark / Barakos, George N. | Wiley | 2017
    Schlagwörter: helicopter rotor blade

    Aerodynamic Design

    Seddon, John / Newman, Simon | Wiley | 2011
    Schlagwörter: blade tip shapes ‐ rotor blade performance, governing entire length , figure‐of‐eight diagrams ‐ for a typical blade , design of rotor blade sections ‐ following lead by fixed‐wing aircraft , Merlin main rotor blade tip (BERP) , incidence and Mach number conditions ‐ rotor blade in forward flight , parasite drag ‐ helicopter parts, fuselage, rotor head, tail rotor and tail surfaces

    Aeroacousto-Elastic Modeling for Response Analysis of Helicopter Rotors

    Gennaretti, Massimo / Bernardini, Giovanni | Springer Verlag | 2012
    Schlagwörter: Rotor Blade , Helicopter Rotor

    Performance

    Seddon, John / Newman, Simon | Wiley | 2011
    Schlagwörter: accurate performance prediction ‐ rotor blade stress, in calculation , helicopter performance assessment ‐ of a fixed‐wing aircraft , shipborne operation benefits ‐ naval helicopter, subject of importance

    Rotor Mechanisms for Forward Flight

    Seddon, John / Newman, Simon | Wiley | 2011
    Schlagwörter: Sikorsky S61NM helicopter ‐ approaching touchdown (coned rotor) , Kaman aircraft, and slightly different system ‐ blade pitch, trailing edge servo flap control , cyclical variation in blade incidence ‐ balancing lift on two sides