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Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed IV : effect of increasing blade speed on velocity diagrams of turbine for engine operation at constant rotative speed (1952)

NASA Technical Reports Server (NTRS) · leaf 20

An illustration from Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed IV : effect of increasing blade speed on velocity diagrams of turbine for engine operation at constant rotative speed, 1952, leaf 20
20 … Turbine exit annular area, Ag, sq in. Figure 3. - Turbine-design requirements for turbine with, fixed rated rotative speed.

NASA Technical Reports Server (NTRS)

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