Preliminary investigation was made of first stage of 2-stage turbine; this stage was matched to centrifugal compressor and operated in conjunction with combustors, engine accessories, and three sizes of jet nozzle.
Investigation of first stage of two-stage turbine designed for free-vortex flow
Nat Advisory Committee Aeronautics -- Tech Note
1950
30 pages
Diagrs, Charts, Tables
Report
English
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Gas Turbine Aero-Engine First Stage Turbine Blade Failure Investigation
Online Contents | 2009
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