Some effects of secondary injection of gases into a supersonic flow
An experimental investigation was conducted in order to determine some of the effects of injection of a secondary stream of gas into a supersonic primary airstream. The flow fields behind an orifice producing essential two-dimensional flow and behind that producing full three-dimensional flow were s...
Internet
https://thesis.library.caltech.edu/3422/1/Burden_hw_1964.pdfBurden, Harvey Worth (1964) Some effects of secondary injection of gases into a supersonic flow. Engineer's thesis, California Institute of Technology. doi:10.7907/DRZK-W405. https://resolver.caltech.edu/CaltechETD:etd-09102002-141125 <https://resolver.caltech.edu/CaltechETD:etd-09102002-141125>