Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/4772
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dc.contributor.authorSaeed, B-
dc.contributor.authorGratton, GB-
dc.date.accessioned2011-03-03T12:07:14Z-
dc.date.available2011-03-03T12:07:14Z-
dc.date.issued2010-
dc.identifier.citationThe Aeronautical Journal, 114(1152): 91-102, Feb 2010en_US
dc.identifier.issn0001-9240-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/4772-
dc.descriptionCopyright @ 2010 The Royal Aeronautical Society. This article is the final author version of the published paper.en_US
dc.description.abstractCombined Vertical and short take-off and landing, or ‘V/STOL’ capability has been of great demand and interest in the field of aeronautics since the creation of the aircraft. V/STOL capability is a targeted capability for many projected or prototype future aircraft. Past V/STOL aircraft are reviewed and analysed with regard to their performance parameters. This research has found two embedded categories in this class of aircraft based on their propulsion systems, i.e. jet and non-jet propulsion, and highlights the significant performance differences between them. In light of historical experience the performance of a relatively new class of aircraft, the flying cars, has been evaluated.en_US
dc.language.isoenen_US
dc.publisherRoyal Aeronautical Societyen_US
dc.rightsCopyright @ 2010 The Royal Aeronautical Society. This article is the final author version of the published paper.-
dc.titleAn evaluation of the historical issues associated with achieving non-helicopter V/STOL capability and the search for the flying caren_US
dc.typeResearch Paperen_US
dc.identifier.doihttps://doi.org/10.1017/s0001924000003560-
Appears in Collections:Mechanical and Aerospace Engineering
Dept of Mechanical and Aerospace Engineering Research Papers

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