DETERMINATION OF THE BASIC PARAMETERS OF VTOL AIRCRAFT WITH VORTEX TYPE LIFTING-TRANSPORTING SYSTEM
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...
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| Format: | Article |
| Language: | Russian |
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Moscow State Technical University of Civil Aviation
2016-12-01
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| Series: | Научный вестник МГТУ ГА |
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| Online Access: | https://avia.mstuca.ru/jour/article/view/884 |
| Summary: | 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. |
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| ISSN: | 2079-0619 2542-0119 |