NASA NTRS · 19900000550
Control-Volume Analysis Of Thrust-Augmenting Ejectors
Abstract
New method of analysis of transient flow in thrust-augmenting ejector based on control-volume formulation of governing equations. Considered as potential elements of propulsion subsystems of short-takeoff/vertical-landing airplanes.
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Drummond, Colin K.. 1990-10-01. Control-Volume Analysis Of Thrust-Augmenting Ejectors. https://ntrs.nasa.gov/citations/19900000550
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