Abstract
The effect of active generation of lift force by an electric impeller propulsion system in integral aerodynamic configurations of vertical take-off and landing aircraft with a flush intake device and an upper step in the stage of start from surface, is shown.
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REFERENCES
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Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2023, No. 3, pp. 51 – 56.
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Ambrozhevich, M.B., Kartashev, A.S., Kornev, A.V. et al. Active Generation of Lift Force in the “Wing–Ejector” Integral Aerodynamic Configuration. Russ. Aeronaut. 66, 469–475 (2023). https://doi.org/10.3103/S1068799823030078
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DOI: https://doi.org/10.3103/S1068799823030078