Silicon Nitride Creep Under Various Specimen-Loading Configurations

By: Nasa, National Aeronautics and Space Adm

Extensive creep testing of a hot-pressed silicon nitride (NC 132) was performed at 1300 C in air using five different specimen-loading configurations: (1) pure tension, (2) pure compression, (3) four-point uniaxial flexure, (4) ball-on-ring biaxial flexure, and (5) ring-on-ring biaxial flexure. This paper reports experimental results as well as test techniques developed in this work. Nominal creep strain and its rate for a given nominal applied stress were greatest in tension, least in compression, and intermediate in uniaxial and biaxial flexure. Except for the case of compression loading, nominal creep strain generally decreased with time, resulting in a less-defined steady-state condition. Of the four creep formulations-power-law, hyperbolic sine, step, and redistribution--the conventional power-law formulation still provides the most convenient and reasonable estimation of the creep parameters of the NC 132 material. The data base to be obtained will be used to validate the NASA Glenn-developed design code CARES/Creep (ceramics analysis and reliability evaluation of structures and creep).Choi, Sung R. and Holland, Frederic A.Glenn Research CenterEXPERIMENT DESIGN; CREEP ANALYSIS; CREEP PROPERTIES; CREEP TESTS; FLEXING; SILICON NITRIDES; RELIABILITY; STEADY STATE

• Format: Paperback
• Language: English
• ISBN: 1723753939
• ISBN13: 9781723753930
• Release Date: January 1
• Publisher: Independently Published
• Length: 38 Pages
• Weight: 0.25 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"