NASA NTRS · 19720023648
A study of nozzle and ejector flow problems by the method of integral relations
Abstract
The application of the method of integral relations to nozzle and ejector flow problems was examined. For nozzle flow problems, the general formulation is that the approaching flow may be rotational. Particular attention was given to the phenomenon of choking under nonuniform flow conditions. Numerical integration of the governing ordinary differential equations was also investigated. This scheme of analysis was also applied to study the interacting flow field within an ejector system.
Keep this discovery
Explore connections, maps & timelines
Howlett, L. D., Chow, W. L.. 1972-06-01. A study of nozzle and ejector flow problems by the method of integral relations. https://ntrs.nasa.gov/citations/19720023648
Cite the original work for its findings. Save a collection to share your selection of sources.