One of most important problems in supersonic range is that of engine control and corresponding control of intake and exhaust geometry by means of pilot's throttle; problem of excessive heating of air intake, and need for cooling of turbine parts to gain increase in thrust; other component problems incident to attainment of speeds of around 2000 mph.
Propulsion problems in high-speed flight
Nature (Lond)
Nature ; 177 , n 4522
1956
4 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
High speed flight propulsion systems
TIBKAT | 1991
|Advanced airbreathing propulsion cycles for high speed flight
Tema Archiv | 1988
|Advanced Airbreathing Propulsion Cycles For High Speed Flight
SAE Technical Papers | 1988
|Engineering Index Backfile | 1956
|Engineering Index Backfile | 1954
|