Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146

Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146
Author: Milton G. Kofskey
Publisher:
Total Pages: 42
Release: 1960
Genre: Liquid propellant rocket engines
ISBN:

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