Thermodynamic data for the calculation of gas turbine performance

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dc.contributor.author D. Fielding en_US
dc.contributor.author J. E. C. Topps en_US
dc.date.accessioned 2014-10-21T15:54:42Z
dc.date.available 2014-10-21T15:54:42Z
dc.date.issued 1954 en_US
dc.identifier.other ARC/R&M-3099 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3671
dc.description.abstract The essential features of a practical method of determining gas turbine performance are that it shall be suitable for accurate routine calculation, and that it is capable of simple modification in order to deal with a range of fuels or with complex cycles. It is the opinion of the authors that the exactitude of the method should also be demonstrable, within the limits imposed by the scales employed, and that it should require only the use of parameters physically intelligible to the average engineer, and a sequence of operations which can be followed by a computer. The calculation should not, moreover, be onerous, involving the use of large or complex charts, or interpolation in tables. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Thermodynamic data for the calculation of gas turbine performance en_US


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