To address the susceptibility of materials used in components of high-performance machinery, such as aircraft engines, to creep (deformation that is induced by persistent mechanical stress and that often occurs at elevated temperatures), materials researchers have developed silicon carbide (SiC) fibers for producing aerospace composites. Testing the thermomechanical properties of several commercially available SiC fibers, Ramakrishna T. Bhatt et al. found that in comparison with two polymer-derived SiC fibers, a nitrogen-treated SiC fiber exhibited a lower minimum creep rate, a measure of the rate at which a stress-exposed material deforms at a constant temperature and uniaxial load. The finding suggests that ______
Which choice most logically completes the text?
Explanation
Context: Bhatt et al. tested SiC fibers and found that a NITROGEN-TREATED SiC fiber had a LOWER MINIMUM CREEP RATE than two polymer-derived SiC fibers. Lower creep rate = deforms more slowly under stress. The blank draws the implication for aerospace composites.
Answer: B) aerospace composites containing the nitrogen-treated SiC fiber may have the ability to withstand mechanical stress for a longer period of time...
Why? Lower creep rate = slower deformation under stress = longer time before failure. B correctly applies this to aerospace composites using the nitrogen-treated fiber.
Traps:
- A) unlike polymer fibers, nitrogen-treated can substantially inhibit creep → the finding shows a comparative difference in RATE, not that polymer fibers can't inhibit creep at all
- C) polymer-derived composites improve stability to greater extent → directly contradicted; nitrogen-treated showed lower (better) creep rate
- D) both polymer fibers hold similar potential → possible, but the finding about nitrogen-treated fiber's advantage doesn't support this specific conclusion