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Conceptual design, evaluation and research identification for Remote Augmented Propulsive Lift Systems (RALS) with ejectors for VTOL aircraftEjector concepts for use with a remote augmented lift system (RALS) exhaust nozzle were studied. A number of concepts were considered and three were selected as having the greatest promise of providing the desired aircraft and exhaust gas cooling and lift enhancement. A scale model test program is recommended to explore the effects of the more important parameters on ejector performance.
Document ID
19830004833
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Willis, W. S. (General Electric Co. Cincinnati, OH, United States)
Konarski, M. (General Electric Co. Cincinnati, OH, United States)
Sutherland, M. V. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-167906
NAS 1.26:167906
R82AEB315
Report Number: NASA-CR-167906
Report Number: NAS 1.26:167906
Report Number: R82AEB315
Accession Number
83N13103
Funding Number(s)
CONTRACT_GRANT: NAS3-22042
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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