NASA NTRS · 19800001878
Nonsteady-Flow Thrust Augmenting Ejectors
Abstract
Ejector augmenters in which the transfer of mechanical energy from the primary to the secondary flow takes place through the work of interface pressure forces are investigated. Nonsteady flow processes are analyzed from the standpoint of energy transfer efficiency and a comparison of a rotary jet augmenter to an ejector is presented.
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Foa, J. V.. 1979-09-01. Nonsteady-Flow Thrust Augmenting Ejectors. https://ntrs.nasa.gov/citations/19800001878
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