Abstract

A facility for the investigation of flow structure in a supersonic combustion chamber has been constructed and tested. The side walls of the rectangular combustion chamber model can be moved during the experiment to the alternately expose water cooled stainless steel or quartz windows. Window exposure time is limited by thermal loading restrictions on the windows. A Schlieren system is used for visualization. Results are presented for tests using both hydrogen fuel and with air being injected through the fuel pylons.

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