Premium
Influence of Loading Frequency on the Room‐Temperature Fatigue of a Carbon‐Fiber/SiC‐Matrix Composite
Author(s) -
Shuler Stephen F.,
Holmes John W.,
Wu Xin,
Roach David
Publication year - 1993
Publication title -
journal of the american ceramic society
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.9
H-Index - 196
eISSN - 1551-2916
pISSN - 0002-7820
DOI - 10.1111/j.1151-2916.1993.tb07772.x
Subject(s) - materials science , composite material , fatigue limit , ultimate tensile strength , composite number , modulus , stress (linguistics) , tension (geology) , fiber , cyclic stress , young's modulus , philosophy , linguistics
The influence of cyclic loading frequency on the tensile fatigue life of a woven‐carbon‐fiber/SiC‐matrix composite was examined at room temperature. Tension‐tension fatigue experiments were conducted under load control, at sinusoidal frequencies of 1, 10, and 50 Hz. Using a stress ratio (σ min /σ max ) of 0.1, specimens were subjected to maximum fatigue stresses of 310 to 405 MPa. There were two key findings: (1) the fatigue life and extent of modulus decay were influenced by loading frequency and (2) the postfatigue monotonic tensile strength increased after fatigue loading. For loading frequencies of 1 and 10 Hz, the fatigue limit (defined at 1 × 10 6 cycles) was approximately 335 MPa, which is over 80% of the initial monotonic strength of the composite; at 50 Hz, the fatigue limit was below 310 MPa. During 1‐ and 10‐Hz fatigue at a maximum stress of 335 MPa, the modulus exhibited an initially rapid decrease, followed by a partial recovery; at 50 Hz, and the same stress limits, the modulus continually decayed. The residual strength of the composite increased by approximately 20% after 1 × 10 6 fatigue cycles at 1 or 10 Hz under a peak stress of 335 MPa. The increase in strength is attributed in part to a decrease in the stress concentrations present near the crossover points of the 0° and 90° fiber bundles.