The component pressure losses in combustion chambers

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dc.contributor.author H. A. Knight en_US
dc.contributor.author R. B. Walker en_US
dc.date.accessioned 2014-10-21T15:54:07Z
dc.date.available 2014-10-21T15:54:07Z
dc.date.issued 1953 en_US
dc.identifier.other ARC/R&M-2987 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3553
dc.description.abstract This Report summarises the available knowledge of the component losses in a combustion chamber. The information given in this Report should enable the pressure drops through swirlers, primary baffles, cooling systems, etc., to be calculated. Most of the data were abstracted and collected from the various reports listed in the bibliography. In certain cases (e.g.,mixing losses) the information is incomplete and in these circumstances the limited experimental results available are supplemented by hypotheses which require proof. A specimen calculation of the pressure drop and airflow distribution of a typical chamber is given in Appendix U. The calculated and measured values of pressure drop (cold) agreed within 4 per cent. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title The component pressure losses in combustion chambers en_US


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