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

Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146 by Milton G. Kofskey PDF Summary

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