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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 37

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 37
CD … CD-5950 Figure 1. - Schematic sketch of engine showing calculation stations. NACA TN 3335 L9V2

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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