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Performance Evaluation of a Two Stage Axial-Flow Turbine for Two Values of Tip Clearance

机译：两级叶尖间隙两级轴流式水轮机性能评价

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作者
Kofskey, M. G.; Nusbaum, W. J.;
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年度 1968
页码 1-2
总页数 2
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Axial flow turbines ; Performance tests ; Tip driven rotors ; Two stage turbines ; Argon ; Clearances ; Fluid dynamics ; Spacing;

机译：轴流式涡轮机;性能测试;尖端驱动转子;两级涡轮机;氩气;间隙;流体动力学;间距;

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3. To a Problem on Distribution of Heat Drop in Two-Stage Axial-Flow Small Turbines with Pressure Stages [J] . N.F. MUSATKIN, V.M. RADKO Известия　Высших　учебных　заведений: Авиационная　техника . 2003,第3期

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4. EFFECTS OF FIRST STAGE TURBINE METAL BLADE TRACK AND TIP CLEARANCE ON FIELDED GAS TURBINE ENGINE PERFORMANCE [C] . Anthony L. Wojtyla, Andrew C. Nix, Phil Reineke, International Symposium on Air Breathing Engines . 2005

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6. Creep-Based Reliability Evaluation of Turbine Blade-Tip Clearance with Novel Neural Network Regression [O] . Chun-Yi Zhang, Jing-Shan Wei, Ze Wang, 2019

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7. Effect of rotor tip clearance and configuration on overall performance of a 12.77-centimeter tip diameter axial-flow turbine [O] . Kofskey, M. G., Haas, J. E. 1978

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8. Performance evaluation of a two stage axial-flow turbine for two values of tip clearance [R] . Kofskey, M. G., Nusbaum, W. J. 1968

机译：两级轴流式涡轮机两尖端间隙值的性能评估

Performance Evaluation of a Two Stage Axial-Flow Turbine for Two Values of Tip Clearance

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