Abstract The work is focused on developing effective systems for the electrogasdynamic control of the boundary layer and gas flows on aerodynamic surfaces. In the course of the research, a new multi-discharge actuator system has been developed that induces a unidirectional and fairly uniform volumetric force effect over the extended aerodynamic surface sections and has significantly better power and energy characteristics than those of well-known world analogues. The experimental validation of weakening the cross-flow in a three-dimensional boundary layer and increasing its stability using a new multi-discharge actuator system has been performed.

    Highlights Multi-discharge actuator system is developed. The system generates unidirectional body force over lengthy aerodynamic surfaces. Body force impact permits to reduce a cross flow in swept wing boundary layer. Cross flow reduction results in attenuation of stationary instability vortices. The laminar-to-turbulent transition is delayed.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Multi-discharge actuator systems for electrogasdynamic flow control



    Published in:

    Acta Astronautica ; 181 ; 292-300


    Publication date :

    2021-01-18


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Corrigendum to “Multi-discharge actuator systems for electrogasdynamic flow control” [Acta Astronaut. 181 (2021) 292–300]

    Khomich, Vladislav Yu. / Yamshchikov, Vladimir A. / Chernyshev, Sergey L. et al. | Elsevier | 2021


    Electrogasdynamic power generation

    GOURDINE, M. C. / KAHN, B. | AIAA | 1964


    Electrogasdynamic laminar flow control on a swept wing

    Chernyshev, Sergey L | Online Contents | 2016


    Pulsed Electrogasdynamic Thruster for In-Space Propulsion

    Nakamura, Takashi / Krech, Robert H. / Smith, Benjamin K. | AIAA | 2020


    ICAS2014_0303: THEORETICAL MODELING OF THE ELECTROGASDYNAMIC METHOD OF LAMINAR FLOW CONTROL ON A SWEPT WING

    Chernyshev, S. L. / Kuryachii, A. P. / Manuilovich, S. V. et al. | British Library Conference Proceedings | 2014