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Rotating primary flow induction using jet-flapped bladesA new concept in ejector design is examined using primary jets exiting from a free spinning bladed rotor. This concept stems from a continuing effort in the development of Rotary-Jet thrust augmentors at George Washington University (GWU). An analysis of a Rotary-Jet rotor with jet-flapped blades is presented, identifying design trends beneficial to its performance. An experimental investigation was conducted to demonstrate the potential of this new concept. Several combinations of blade and shroud geometries were designed, fabricated and tested. The results are presented and discussed. Despite crudeness of fabrication, the maximum thrust augmentations obtained ranged from 1.55 to 2.14. These results demonstrate that this device is superior to all ejector designs tested with similar conventional passive diffusing shrouds.
Document ID
19900025530
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cordier, Stephane J.
(George Washington University Washington, DC, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aircraft Propulsion And Power
Accession Number
90A12585
Funding Number(s)
CONTRACT_GRANT: NAG3-860
CONTRACT_GRANT: DOT-MA91-85-C-50114
Distribution Limits
Public
Copyright
Other

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