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 PDF book is popular Liquid propellant rocket engines book written by Milton G. Kofskey. The book was released by on 1960 with total hardcover pages 42. Fast download link is given in this page, you could read Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146 by Milton G. Kofskey in PDF, epub and kindle directly from your devices.
Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146
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Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146 Book Detail
- Author : Milton G. Kofskey
- Release Date : 1960
- Publisher :
- Genre : Liquid propellant rocket engines
- Pages : 42
- ISBN 13 :
- File Size : 8,8 MB