Abstract
An experimental investigation of the operating characteristics of a two-dimensional planar, constant area, supersonic-subsonic ejector with a steady or a periodically pulsed continuous driver flow is presented. Improvements in ejector pressure recovery and entrainment capabilities resulted from the periodic driver for a limited range of operating conditions.
Original language | English (US) |
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Pages (from-to) | 1851-1852 |
Number of pages | 2 |
Journal | AIAA journal |
Volume | 23 |
Issue number | 12 |
DOIs | |
State | Published - Dec 1985 |
ASJC Scopus subject areas
- Aerospace Engineering