Publication Date:
2016-06-07
Description:
The beneficial aspects of an ejector powered V/STOL concept were reviewed. The feasibility of satisfactorily incorporating an ejector system in a high performance V/STOL aircraft was investigated. The external augmentor concept, based on the use of chordwise ejector slots, is presented. It is concluded that the external augmentor concept has a basic inherent simplicity and a sufficient augmentor performance potential to make feasible a high performance V/STOL aircraft based on ejectors.
Keywords:
AERODYNAMICS
Type:
NASA. Ames Res. Center Workshop on Thrust Augmenting Ejectors; p 449-471
Format:
application/pdf
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