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Method for Rapid Graphical Evaluation of Cooled or Uncooled Turbojet and Turboprop Engine or Component Performance (effects of Variable Specific Heat Included) (1955)

NASA Technical Reports Server (NTRS) · leaf 43

An illustration from Method for Rapid Graphical Evaluation of Cooled or Uncooled Turbojet and Turboprop Engine or Component Performance (effects of Variable Specific Heat Included), 1955, leaf 43
Figure 7. - Turbine work and temperature ratio. (A large working copy of this chart may be obtained by using the request card bound In the back of the report.)

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