A Preliminary Design Analysis of a Multi-Channel Ejector Thrust Augmentation Concept with Oval or Rectangular Air Supply Ducts

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Report Number: ARL 72-0062
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
Pages: 77
Contract: F33615-71-C-1802
DoD Project: 7116
DoD Task:
Identifier: AD0744839
AD Number: AD 744839

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Provenance: Bombardier/Aero

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