Basic requirements and design considerations; propulsion system conceived for high speed VTOL aircraft by Aircraft Gas Turbine Div, General Electric, Evendale, Ohio; conventional turbojet sized so it will produce adequate cruise thrust at moderate altitudes and attractive subsonic speeds; lift fan is driven by engine which is shut down during cruise; specific convertible VTOL aircraft design.
Some thoughts on VTOL propulsion
Am Helicopter Soc -- J
American Helicopter Society -- Journal ; 4 , n 1
1959
6 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1965
|Propulsion spectrum for VTOL aircraft
Engineering Index Backfile | 1959
|Cycloidal Propulsion for UAV VTOL Applications
NTIS | 1998
|A PROPULSION SPECTRUM FOR VTOL AIRCRAFT
SAE Technical Papers | 1959
|Ducted Propulsion Units for VTOL Aircraft
NTIS | 1968
|