DETERMINATION OF THE BASIC PARAMETERS OF VTOL AIRCRAFT WITH VORTEX TYPE LIFTING-TRANSPORTING SYSTEM
Abstract
The article deals the results of calculating the basic parameters of VTOL aircraft, that has the vortex liftingtransporting system, based on the use of an aerodynamic effect of Magnus. Calculations showed that at the contemporary level of aircraft construction development it is possible to create a flight vehicle of such type, with takeoff mass about 120 tons, range and flight speed respectively 7000 km and 400 km/h.
About the Author
L. V. Mikhnenkov
Российская академия космонавтики им. Циолковского
Russian Federation
Russian Federation
References
1. Mihnenkov L.V. Aviacionnaja podjomno-transportnaja sistema i vetrojenergeticheskie ustrojstva vihrevogo tipa. Monografija. M.: MGTUGA, 2014.
Review
For citations:
Mikhnenkov L.V. DETERMINATION OF THE BASIC PARAMETERS OF VTOL AIRCRAFT WITH VORTEX TYPE LIFTING-TRANSPORTING SYSTEM. Civil Aviation High Technologies. 2016;(225):117-123. (In Russ.)
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