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COMPUTATION OF TEMPERATURE FIELDS AND STRESSES IN THE COOLED ROTOR OF A GAS TURBINE ON STARTING

机译：启动时燃气轮机冷却转子中温度场和应力的计算

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摘要

A method is presented for the calculation of temperatures and stresses in the disks of gas turbines on starting, by means of a universal program for the "Ural-l" electronic digital computer.

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作者
S. A. Moktushin; Ya. M. Gusak;
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年度 1965
页码 1-23
总页数 23
原文格式 PDF
正文语种 eng
中图分类工业技术;
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4. INTERVAL ARITHMETIC BASED GRAY MODEL ON THERMAL STRESSES FIELD COMPUTATION OF TURBINE ROTOR [C] . Zhou Yuyang, Chen Hanping, Fan Jun CSPE-JSME-ASME International Conference on Power Engineering Vol.1 Oct 8-11, 2001, Xi'an, China . 2001

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5. Experimental Investigation of the Effect of Engine Representative Combustor Exit Temperature Profile and Disc Cavity Leakage Flow on the Film Cooling of Contoured Hub Endwall of a High Pressure Gas Turbine Rotor Cascade. [D] . Ayaskanta, Arya. 2013

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COMPUTATION OF TEMPERATURE FIELDS AND STRESSES IN THE COOLED ROTOR OF A GAS TURBINE ON STARTING

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