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An Investigation of Ejectors Having Short Mixing Sections
ISSN: 0148-7191, e-ISSN: 2688-3627
Published January 01, 1964 by SAE International in United States
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A complete description and discussion of an ejector model test program is given. Specific parameters investigated experimentally and discussed are: (1) primary steam supply pressure and temperature; (2) primary steam expansion ratio; (3) type, temperature, and mode of injection of secondary gas; and (4) geometry of ejector. Where possible, the experimental results are compared with other data and theoretical analysis. Conclusions are drawn as to the general design criteria for short ejectors.
CitationHaroldsen, O., "An Investigation of Ejectors Having Short Mixing Sections," SAE Technical Paper 640284, 1964, https://doi.org/10.4271/640284.
- Nelson R. E. Patmor G. O. McFarland B. L. Mandell B. “Scale Model Testing of 90° Turn Ejector Systems for Rocket Engine Altitude Simulation,” AIAA Summer Meeting Los Angeles, California June 1963
- Haroldsen O. O. “Ejector Model Test Program for J-2 Altitude System,” May 1964