ZENG Chuan, WANG Hong-ming, SHAN Peng. The Design and Study of the Annular Combustion Chamber with Centrifugal Fuel Injection[J]. Journal of Aerospace Power, 2003, 18(1): 92-96.
Citation:
ZENG Chuan, WANG Hong-ming, SHAN Peng. The Design and Study of the Annular Combustion Chamber with Centrifugal Fuel Injection[J]. Journal of Aerospace Power, 2003, 18(1): 92-96.
ZENG Chuan, WANG Hong-ming, SHAN Peng. The Design and Study of the Annular Combustion Chamber with Centrifugal Fuel Injection[J]. Journal of Aerospace Power, 2003, 18(1): 92-96.
Citation:
ZENG Chuan, WANG Hong-ming, SHAN Peng. The Design and Study of the Annular Combustion Chamber with Centrifugal Fuel Injection[J]. Journal of Aerospace Power, 2003, 18(1): 92-96.
For most micro turbojet layouts,the annular combustion chamber shows itself as one of the best combustion system arrangements.It can usually be shown to be the lightest,least expensive to manufacture,and most efficient combustion system arrangement in terms of utilization of the specified engine volume.In this paper,the design and study of the annular combustion chamber with centrifugal fuel injection are presented.
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