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Analytical investigation of performance of two-stage turbine over a range of ratios of specific heats from 1.2 to 1 2/3 Warren J. Whitney and Warner L. Stewart.

Title:Analytical investigation of performance of two-stage turbine over a range of ratios of specific heats from 1.2 to 1 2/3 Warren J. Whitney and Warner L. Stewart.
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Note:National Aeronautics and Space Administration :, 1962
  
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Subject:Aerodynamics, missiles and space vehicles
Subject:Propulsion systems, air-jet
Subject:Propulsion systems, electric
Subject:Propulsion systems, liquid-fuel rockets
Subject:Turbines -- Effect of high temperatures on -- Analysis
Subject:Turbines -- Models -- Testing
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