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An Investigation of Ejectors Having Short Mixing Sections
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English
Abstract
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.
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Citation
Haroldsen, O., "An Investigation of Ejectors Having Short Mixing Sections," SAE Technical Paper 640284, 1964, https://doi.org/10.4271/640284.Also In
References
- 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