A feasibility assessment of annular winged VTOL flight vehicles

B. Saeed*, G. B. Gratton, C. Mares

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

This paper presents a feasibility study to integrate a developed lift system (an annular wing wrapped around a centrifugal flow generator) into a Vertical/Short Take-Off and Landing V/STOL aircraft. Different physical scales, from micro aerial vehicle to a Harrier Jump Jet scale, for a variety of propulsion systems are explored. The system has shown to be viable for several classes of aircraft but with better performance offered by a micro-aerial-vehicle (~ 40g) and a large vehicle (~ 10,000 kg) with a turbofan engine, albeit in both cases with apparently worse performance than is offered by current technologies. The wingform does not appear to be feasible in the light aircraft scale whilst using internal combustion engines.
Original languageEnglish
Article number3703
Pages (from-to)683-692
Number of pages9
JournalThe Aeronautical Journal
Volume115
Issue number1173
DOIs
Publication statusPublished - Nov 2011

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