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Design and Experimental Analysis of Aircrew Design Parameters to Vertical Takeoff and Landing

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Abstract

The calculation of the design parameters of lifting airscrew systems with fixed and tilted rotor, including the investigation of the operation schemes of actuators for the propeller control system, is carried out.

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Authors and Affiliations

  1. Kazan (Volga region) Federal University, ul. Kremlevskaya 18, Kazan Tatarstan, 420008, Russia

    T. Yu. Gainutdinova

  2. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10 Tatarstan, Kazan, 420111, Russia

    V. G. Gainutdinov

Authors
  1. T. Yu. Gainutdinova
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  2. V. G. Gainutdinov
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Corresponding author

Correspondence to T. Yu. Gainutdinova.

Additional information

Original Russian Text © T.Yu. Gainutdinova, V.G. Gainutdinov, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 1, pp. 11–16.

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Gainutdinova, T.Y., Gainutdinov, V.G. Design and Experimental Analysis of Aircrew Design Parameters to Vertical Takeoff and Landing. Russ. Aeronaut. 61, 8–13 (2018). https://doi.org/10.3103/S1068799818010026

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  • DOI: https://doi.org/10.3103/S1068799818010026

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