1–11 of 11 hits
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    Numerical investigation of blade-tip-vortex dynamics

    Kaufmann, Kurt / Wolf, C. Christian / Merz, Christoph B. et al. | Online Contents | 2018
    Keywords: Blade-tip-vortex , Helicopter blade

    Numerical investigation of the vortex roll-up from a helicopter blade tip using a novel fixed-wing adaptation method

    Joulain, Antoine / Desvigne, Damien / Alfano, David et al. | Online Contents | 2017
    Keywords: Blade tip , Helicopter

    Experimental investigation of high-pressure pulsed blowing for dynamic stall control

    Gardner, A. D. / Richter, K. / Mai, H. et al. | Online Contents | 2014
    Keywords: Helicopter Blade Wind tunnel

    Aerodynamic design optimization of a helicopter rotor blade-sleeve fairing

    Pölzlbauer, P. / Desvigne, D. / Breitsamter, C. | Online Contents | 2018
    Keywords: Blade-sleeve fairing , Helicopter aerodynamics

    Reduction of dynamic stall using a back-flow flap

    Gardner, A. D. / Opitz, S. / Wolf, C. C. et al. | Online Contents | 2017
    Keywords: Helicopter blade

    About the impact of wind turbine blade tip vortices on helicopter rotor trim and rotor blade motion

    van der Wall, Berend G. / Lehmann, Paul H. | Online Contents | 2017
    Keywords: Rotor blade motion , Helicopter rotor trim

    Characterization and selection of basic parameters for steering servo of a small remotely-piloted single-rotor helicopter with tail rotor

    D’yakonov, D. A. / Zavalov, O. A. / Kuptsov, D. A. et al. | Online Contents | 2014
    Keywords: remotely piloted helicopter , rotor blade , tail rotor blade

    Approximate technique of tip vortex account in calculating a helicopter main rotor

    Liss, A. Yu. | Online Contents | 2012
    Keywords: helicopter main rotor , varying blade loads

    Aerodynamic and structural investigation of an active back-flow flap for dynamic stall control

    Opitz, S. / Gardner, A. D. / Kaufmann, K. | Online Contents | 2014
    Keywords: Helicopter , Rotor blade

    A lower bound estimate of the critical load for helicopter main rotor composite blade according to the limit equilibrium theory. Analysis results

    Gorelov, A. V. / Sidorov, I. N. | Online Contents | 2011
    Keywords: helicopter main rotor , composite blade