Results of work on ejector problem carried out at United Aircraft Corp; equations developed which enable estimation of performance of steady flow ejectors pumping fluid across small pressure rise or drop; principal uses for ejector engine installations are in those cases in which cooling would otherwise have to be obtained by use of fan or stalled cowl flaps, or in which exhaust thrust could not otherwise be used because of flame, noise, or temperature.
Aircraft ejector performance
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 13 , n 11
1946
10 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.