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A Preliminary Design Analysis of a Multi-Channel Ejector Thrust Augmentation Concept with Oval or Rectangular Air Supply Ducts
Author(s): Wright, D. C., Allen, J. G., Meholick, W. N., Salter, G. R., Ashby, R., Tilyou, C.Corporate Author(s): Bell Aerospace Company
Laboratory: Aerospace Research Laboratories
Date of Publication: 1972-05
Report number: ARL 72-0062
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