Ejector-Nozzle Flow and Thrust for Choked Flow
Copyright policy ) H. E. Weber;
Ejector-Nozzle Flow and Thrust for Choked Flow
A theory for the prediction of flow for fully choked divergent shroud nozzles has been compared with experiment and corrected empirically. The prediction of thrust has been extended to include both the underexpanded and overexpanded flow regimes in this type of nozzle. Comparisons with the theory have been made and good correlation found in both overexpanded and underexpanded regimes of flow.
- Ericsson (Sweden) Sweden
- Space Sciences Laboratory United States
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These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
Citations provided by BIP!popularityPopularity provided by BIP!
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
Popularity provided by BIP! 1
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