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On One Approach to Design of the Rudder-Drive System Taking into Account the Aeroelastic Stability Requirements

  • Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
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Abstract

An approach to design of the rudder—drive system taking into account the aeroelastic characteristics of the rudder is proposed. Mathematical models are developed that are used to solve problems of the rudder design parameters selection and the rudder—drive system stability analysis. An example of design of the rudder—drive system of the air-to-air unmanned aerial vehicle is given.

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Authors and Affiliations

  1. Moscow Aviation Institute, National Research University, Volokolamskoe sh. 4, Moscow, 125993, Russia

    S. G. Parafes’ & I. K. Turkin

Authors
  1. S. G. Parafes’
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  2. I. K. Turkin
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Correspondence to S. G. Parafes’.

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Russian Text © The Author(s), 2020, published in Izvestiya Vysshikh Uchebhnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 1, pp. 71–77.

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Parafes’, S.G., Turkin, I.K. On One Approach to Design of the Rudder-Drive System Taking into Account the Aeroelastic Stability Requirements. Russ. Aeronaut. 63, 75–82 (2020). https://doi.org/10.3103/S1068799820010109

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  • DOI: https://doi.org/10.3103/S1068799820010109

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