Effects of injection nozzle configuration on secondary injection into supersonic flow

Effects of injection nozzle configuration on secondary injection into supersonic flow

<p>Gaseous nitrogen and argon were injected into a primary stream of air moving at Mach 2.56. The gases were injected at secondary to primary total pressure ratios from 3.2 to 28.6 through four different nozzles. Two nozzles, one sonic and one supersonic (M = 3.26), injected normal to the pr...

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Bibliographic Details
Main Author: Street, Donald Richard
Format: Others
Published: 1966
Online Access:https://thesis.library.caltech.edu/9245/1/Street_dr_1966.pdf
Street, Donald Richard (1966) Effects of injection nozzle configuration on secondary injection into supersonic flow. Engineer's thesis, California Institute of Technology. doi:10.7907/WZWF-JK12. https://resolver.caltech.edu/CaltechTHESIS:10262015-092430262 <https://resolver.caltech.edu/CaltechTHESIS:10262015-092430262>

Internet

https://thesis.library.caltech.edu/9245/1/Street_dr_1966.pdf
Street, Donald Richard (1966) Effects of injection nozzle configuration on secondary injection into supersonic flow. Engineer's thesis, California Institute of Technology. doi:10.7907/WZWF-JK12. https://resolver.caltech.edu/CaltechTHESIS:10262015-092430262 <https://resolver.caltech.edu/CaltechTHESIS:10262015-092430262>

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