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    Experimental research of single - rotor helicopter unintentional yaw rotation

    Free access
    V. V. Efimov / V. A. Ivchin / O. E. Chernigin et al. | DOAJ | 2020

    Development of the technical solution to prevent a single-rotor helicopter from entering uncontrolled rotation

    Free access
    V. A. Ivchin / K. Y. Samsonov / A. M. Kasimov et al. | DOAJ | 2022

    THE EFFECT OF DIFFERENT OPTIONS OF BLADES MAIN ROTOR ON THE X-SHAPED TAIL ROTOR OF THE MI-171 LL

    Free access
    V. A. Ivchin / V. A. Nikiforov / K. Yu. Samsonov | DOAJ | 2018

    IMPACT OF AN UNDERSLUNG LOAD ON A HELICOPTER CONTROLLABILITY

    Free access
    G. N. Babenko / V. V. Efimov / V. A. Ivchin | DOAJ | 2017

    RESULTS OF THE FIRST MI-171A2 FLYING LABORATORY TEST PHASE

    Free access
    V. A. Ivchin / K. Y. Samsonov | DOAJ | 2016

      RESULTS OF THE FIRST MI-171A2 FLYING LABORATORY TEST PHASE

      Free access
      V. A. Ivchin / K. Y. Samsonov | DOAJ | 2014

    COMPARATIVE STUDY ON CALCULATION RESULTS OF THREE-BLADE AND X-SHAPED TAIL ROTOR AT "VORTEX RING"

    Free access
    Y. M. Ignatkin / P. V. Makeev / A. I. Shomov et al. | DOAJ | 2016

    RESEARCH OF AREAS OF DANGEROUS COMBINATION "HEIGHT - FLIGHT SPEED" FOR GYROPLANE

    Free access
    V. A. Ivchin | DOAJ | 2015