Description
This work describes the numerical process developed for use of rocket engine nozzle ejectors. Ejector nozzles, while applied to jet engines extensively, have not been applied to rockets, and have great potential to improve the performance of endoatmospheric rocket propulsion systems.
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Contributors
- Gibson, Gaines Sullivan (Author)
- Wells, Valana (Thesis director)
- Takahashi, Timothy (Committee member)
- Barrett, The Honors College (Contributor)
- Mechanical and Aerospace Engineering Program (Contributor)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2014-05
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