An evaluation of the historical issues associated with achieving non-helicopter V/STOL capability and the search for the flying car
Author(s)
Saeed, B
Gratton, GB
Type
Journal Article
Abstract
Combined 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.
Date Issued
2010-02
Date Acceptance
2016-02-01
Citation
The Aeronautical Journal, 2010, 114 (1152), pp.91-102
ISSN
0001-9240
Publisher
Cambridge University Press (CUP)
Start Page
91
End Page
102
Journal / Book Title
The Aeronautical Journal
Volume
114
Issue
1152
Copyright Statement
Copyright © Royal Aeronautical Society 2010. This article has been published in a revised form in The Aeronautical Journal https://doi.org/10.1017/S0001924000003560. This version is free to view and download for private research and study only. Not for re-distribution, re-sale or use in derivative works.
Identifier
http://dx.doi.org/10.1017/s0001924000003560
Subjects
09 Engineering
15 Commerce, Management, Tourism and Services
Aerospace & Aeronautics
Publication Status
Published
Date Publish Online
2016-02-03