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Design of Radial Inflow and Mixed Flow Turbines 1971

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Design of Radial Inflow and Mixed Flow Turbines 1971 ( design-radial-inflow-and-mixed-flow-turbines-1971 )

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COhTENTS 2. Steady Flow (Constant Pressure) Analysis (a) (b) (0) Pulse Flow Analysis Unchoked Nozzle Choked Nozzle Two lhtry Casing 3. 4. Three-Dimensional and Plotting Programme Page 2 1. Introduction Notation References Illustrations - Figures q-lob Detachable Abstract Cards 1. INTRODUCTION Over the last 12 years, intensive work on radial inflow turbines has been proceeding under the writer's direotion, arising out of the need to design a turbine for road traction applications operating in association with a free piston gas generator delivering gas at 4 bar (approx) and 450%. This early work (1958) led to the formulation of a simple, but nevertheless then unique, treatment covering, by one dimensional methods, both design and. off design conditions, as well as a rapid prediction technique for blade to blade pressure and velocity gradients in terms of mid-channel values of velocities and geometric properties, and derived values of the tangential acceleration (Reference 1). This treatment was later extended to analyse pulsating flow conditions in radial flow turbines, using the method of characteristics duct, volute the two sets equations in to formulate equations for wave propagation in the supply and nozzle ring, on the one hand, and the rotor on the other, of conditions being joined by continuity, momentum and energy the interspace allowing for entropy gain (References 2, 3 and 4). A largely experimental attack on the problem was reported separately in Reference 5. Reference 2 dealt exclusively with single entry turbines, whilst References 3 and 4 cover the cases of multi entry casings using either the full unsteady or a simpler quasi steady treatment.

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