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Turbine Engines for High-Speed Flight

Hugh M. Henneberry, A. V. Zimmerman

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Abstract

This analysis investigates the application of gas turbine engines at a cruise Mach number of 4. Some of the problems of turbine engines, including cooling and off-design performance of certain components, are explored and feasible solutions to the problems are demonstrated.

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What this paper is about

This analysis investigates the application of gas turbine engines at a cruise Mach number of 4. Some of the problems of turbine engines, including cooling and off-design performance of certain components, are explored and feasible solutions to the problems are demonstrated.

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Method / approach

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Available abstract

This analysis investigates the application of gas turbine engines at a cruise Mach number of 4. Some of the problems of turbine engines, including cooling and off-design performance of certain components, are explored and feasible solutions to the problems are demonstrated.

Key concepts: Aeronautics, Turbine, Aerospace engineering, Automotive engineering, Engineering, Computer science

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