Outline of Bristol Siddeley's views on strike aircraft design summarized; with experience gained of jet lift aircraft powered by single lift/thrust turbofan or composite installation of specialized lifting and propulsion engines, it is appropriate to consider characteristics required of engines for next generation of low level strike aircraft having supersonic capability; engine thermodynamics for supersonic strike aircraft; aircraft characteristics; choice of lift/thrust engine characteristics and of characteristics for specialized lifting and propulsion engines; advantages of lift/thrust engines.
VTOL power
Flight
Flight ; 83 , n 2809
1963
2 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
VTOL aircraft control power costs
AIAA | 1971
|VTOL control power requirements reappraised.
AIAA | 1966
|VTOL ELECTRIC POWER SYSTEM ARCHITECTURE AND FAULT TOLERANT VTOL AIRCRAFT USING SAME
European Patent Office | 2024
|Power plants for VTOL aircraft
Engineering Index Backfile | 1957
|