Aerodynamic Calculation of Blades in Axial-Flow Turbomachines,
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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The report discusses the direct and inverse problems of calculating the stages of axial turbine machines within the framework of the theory of cylindrical and conical stages with consideration of blockage of the flow by the blades and of the slope and curvature of the meridian lines of the current. A mathematical formulation is presented for these problems along with methods of solving them on the electronic computer and manually.
- Jet and Gas Turbine Engines