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Author by: William R. Hawthorne Language: en Publisher by: Princeton University Press Format Available: PDF, ePub, Mobi Total Read: 60 Total Download: 455 File Size: 41,8 Mb Description: Volume XI of the High Speed Aerodynamics and Jet Propulsion series. Edited by W.R. Hawthorne and W.T. This is a comprehensive presentation of basic problems involved in the design of aircraft gas turbines, including sections covering requirements and processes, experimental techniques, fuel injection, flame stabilization, mixing processes, fuels, combustion chamber development, materials for gas turbine applications, turbine blade vibration, and performance. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press.

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Stressing basic theory, it offers an authorative source of information on the design of the components, the calculation, analysis, and prediction of performance, the correction of test results, and the presentation of performance data. Much of the material applies to stationary as well as to aircraft power plants. The book concentrates on fundamental principles which are important regardless of changes in design details and adopts throughout the practice of expressing equations in terms of the isentropic factor X. This method results in considerable simplification of equations and greater ease of calculation (tables of X are provided in text).