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A laminar flow rotor for a radial inflow turbine
29th Joint Propulsion Conference and Exhibit, 1993The state of the boundary layers on the blade surfaces of the rotor of a radial inflow turbine has been investigated using surface-mounted hot-film anemometers. The boundary layers are shown to be laminar or intermittently turbulent at the design flow condition.
I. Huntsman, H. P. Hodson
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A cooled laminated radial turbine technology demonstration
18th Aerospace Sciences Meeting, 1980A low-cost, high-temperature radial turbine has been developed demonstrating the technology required to manufacture a small, cooled turbine using photoetched laminates bonded together to form a complete wheel. An advanced long-life, high-performance turbine design is described which uses an iterative optimization procedure to provide a balanced ...
Roy W. Vershure +3 more
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1984
The flow path in radial turbines may be centrifugal as in the Ljungstrom design or, more commonly, centripetal as in most of the machines found in both water power installations and in gas power generation plant. The two types of flow path are illustrated in Figs 8.1, 8.2 and 8.3.
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The flow path in radial turbines may be centrifugal as in the Ljungstrom design or, more commonly, centripetal as in most of the machines found in both water power installations and in gas power generation plant. The two types of flow path are illustrated in Figs 8.1, 8.2 and 8.3.
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The Radial Turbine as a Ceramic Component
Volume 1B: General, 1978In sizes suitable for automotive gas turbines, the small radial turbine has component efficiency equal to that of the axial type, is less sensitive to the effects of tip clearance, and translates more readily into the ceramic medium with minimal aerodynamic compromise.
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Axial and Radial Turbines for Gases
2015Fundamentals of axial turbines were discussed in the chapter on steam turbines (Chap. 6). Design of turbine parts in gas turbines follows the same principles. When analysing the performance of axial turbines, we assumed, by way of a simplification, a given stator outlet angle (α 1 = 72° and 75°).
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Radial-Flow Compressors and Turbines for the Simple Small Gas Turbine
Journal of Fluids Engineering, 1952Abstract This paper describes the procedure followed in developing an acceptable radial-flow turbine for use with a lightweight gas-turbine-driven fire pump for the Navy Bureau of Ships. In the course of this work considerable data were accumulated on general design information and practice on radial compressors and turbines. A review is
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