Low-Cycle Fatigue Analysis of the Turbine Disk for the National Aeronautics and Space Administration High-Temperature Turbine Rig / S. Tepper
- Conference Author:
- Thermal Fatigue of Materials and Components (1975 : New Orleans)
- Physical Description:
- 1 online resource (17 pages) : illustrations, figures, tables
- Additional Creators:
- Tepper, S.
American Society for Testing and Materials
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- The high-pressure, high-temperature turbine test rig was designed for the National Aeronautics and Space Administration to test turbine components in an environment that simulates current and future gas turbines operating at 41 atm (600 psi) and 2204¿̐ưC (4000¿̐ưF). This paper illustrates the design approach that led to selection of a typical test rig component: the turbine disk. The final configuration of the rotor assembly and the turbine disk was determined by analysis of low-cycle fatigue and creep.
- Dates of Publication and/or Sequential Designation:
- Volume 1976, Issue 612 (January 1976)
- Digital File Characteristics:
- text file PDF
- Bibliography Note:
- Includes bibliographical references 9.
- Other Forms:
- Also available in PDF edition.
Also available online via the World Wide Web. Tables of contents and abstracts freely available; full-text articles available by subscription.
Full text article also available for purchase.
- Reproduction Note:
- Electronic reproduction. W. Conshohocken, Pa. : ASTM International, 1976. Mode of access: World Wide Web. System requirements: Web browser. Access may be restricted to users at subscribing institutions.
- Technical Details:
- Mode of access: World Wide Web.
- Source of Acquisition:
- ASTM International PDF Purchase price USD25.
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