Loginov V, Ukrainets Y, Kravchenko I, Yelanskiy A. Experimental research into aerodynamic characteristics of a nacelle with the enabled system of engine thrust neutralization. EEJET [Internet]. 2018Nov.22 [cited 2024Dec.23];6(8 (96):65-73. Available from: https://journals.uran.ua/eejet/article/view/147986