Vertical Take-off Devices with Jet-Vortex Lift Generators
https://doi.org/10.30932/1992-3252-2019-17-1-46-57
Abstract
A theoretical and calculational substantiation of a possibility of implementing a qualitatively new design scheme of an aircraft of vertical take-off, in which the lifting force is initiated by a single vortex, artificially created over the aircraft, and the resulting static pressure drop above and below the device is presented. Decisions on vortex flows generated by a rotating disk and tornado-like vortexes arising in the atmosphere are analyzed. Layout schemes of an apparatus for vertical take-off of two types are proposed - with vortex and jet-vortex lift generators. In both schemes, it is supposed to use vertically mounted bi-rotor drive motors, in which both the rotor and the stator rotate, but in mutually opposite directions.
About the Authors
N. N. OstroukhovRussian Federation
Ostroukhov, Nikolai N. - Ph.D. (Physics and Mathematics), senior lecturer, associate professor of the department of Theoretical Electrical Engineering
E. V. Chumakova
Russian Federation
Chumakova, Ekaterina V. - Ph.D. (Physics and Mathematics), associate professor of the department of Computer mathematics MAI
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Review
For citations:
Ostroukhov N.N., Chumakova E.V. Vertical Take-off Devices with Jet-Vortex Lift Generators. World of Transport and Transportation. 2019;17(1):46-57. https://doi.org/10.30932/1992-3252-2019-17-1-46-57