cannular combustion chambers

cannular combustion chambers

[′kan·yə·lər kəm′bəs·chən ‚chām·bərz]
(aerospace engineering)
The separate combustion chambers in an aircraft gas turbine. Also known as can-type combustors.
McGraw-Hill Dictionary of Scientific & Technical Terms, 6E, Copyright © 2003 by The McGraw-Hill Companies, Inc.
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