Performance Evaluation Of A Two Stage Turbine Designed For A Ratio Of Blade Speed To Jet Speed Of 0146
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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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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the N
