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person:(Popov, S.)

    Effect of Surface Heat Exchange Intensifier Geometry on Heat Transfer Tube Strength

    Popov, I. A. / Shchelchkov, A. V. / Aksyanov, R. A. et al. | Online Contents | 2019

    Development of an SPT-100VT Stationary Plasma Thruster with Increased Thrust

    Kim, V. P. / Gnizdor, R. Yu. / Grdlichko, D. P. et al. | Online Contents | 2019

    Definition of Wingtip Devices Shape and Dimensions for a Subsonic Airliner

    Gueraiche, D. / Popov, S. A. / Ryzhov, Yu. A. | Online Contents | 2018

    Numerical Determination of Contact Forces in Radial Roller Bearings with Flexible Rings

    Ivannikov, V. V. / Degtyarev, S. A. / Popov, V. V. et al. | Online Contents | 2018

    Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems

    Bogatyi, A. V. / El’nikov, R. V. / Nazarenko, I. P. et al. | Online Contents | 2018

    Experimental study of the aerodynamics of a wing with various configurations of wingtip triangular extension

    Popov, S. A. / Djahid, Gueraiche / Kuznetsov, A. V. | Online Contents | 2016

    Model refinements and experimental testing of highly flexible piezoelectric energy harvesters

    Patel, R | Online Contents | 2016
    Beteiligte: McWilliam, S , Popov, A.A

    A hybrid model of hypersonic flow

    Ryzhov, Yu. A. / Nikitchenko, Yu. A. / Popov, S. A. | Online Contents | 2015