STOL Capabilities of VTOL Aircraft – Some Operating Parameters

640305

01/01/1964

Event
SAE World Congress & Exhibition
Authors Abstract
Content
Data reported here show that the military VTOL aircraft is limited to short ranges and small loads, and hence it is important to consider its overloaded performance. General curves show effects of power loading and wing lift on takeoff performance. It is suggested that a variable sweep wing will overcome conflicting requirements. The variation of interference effects with engine position and forward speed is shown. The pilot techniques used during a short take-off and some of the engineering work carried out on variable sweep wings are illustrated.
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DOI
https://doi.org/10.4271/640305
Pages
8
Citation
Boorer, N., and Davey, B., "STOL Capabilities of VTOL Aircraft – Some Operating Parameters," SAE Technical Paper 640305, 1964, https://doi.org/10.4271/640305.
Additional Details
Publisher
Published
Jan 1, 1964
Product Code
640305
Content Type
Technical Paper
Language
English