This analysis investigates the application of gas turbine engines at a cruise Mach number of 4

Henneberry, H. M.

Zimmerman, A. V.

English

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

Turbine Engines for High-Speed Flight

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