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![Effects of Prior Aging at 191°C on Creep Response of IM7/BMI 5250-4]( "Effects of Prior Aging at 191°C on Creep Response of IM7/BMI 5250-4")
Effects of Prior Aging at 191°C on Creep Response of IM7/BMI 5250-460,99 €![Some Aspects of the Mechanical Response of BMI 5250-4 Neat Resin at 191 C: Experiment and Modeling]( "Some Aspects of the Mechanical Response of BMI 5250-4 Neat Resin at 191 C: Experiment and Modeling")
Some Aspects of the Mechanical Response of BMI 5250-4 Neat Resin at 191 C: Experiment and Modeling60,99 €![Effects of Prior Aging At 288°C in Argon Environment on Creep Response of Carbon Fiber Reinforced PMR-15 Composite with ±45° Fiber Orientation at 288°]( "Effects of Prior Aging At 288°C in Argon Environment on Creep Response of Carbon Fiber Reinforced PMR-15 Composite with ±45° Fiber Orientation at 288°")
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Extension of Viscoplasticity Based on Overstress to Capture the Effects of Prior Aging on the Time Dependent Deformation Behavior of a High-Temperatur63,99 €![Fatigue Behavior of an Advanced Sic/Sic Composite with an Oxidation Inhibited Matrix at 1200°C in Air and in Steam]( "Fatigue Behavior of an Advanced Sic/Sic Composite with an Oxidation Inhibited Matrix at 1200°C in Air and in Steam")
Fatigue Behavior of an Advanced Sic/Sic Composite with an Oxidation Inhibited Matrix at 1200°C in Air and in Steam61,99 €![Fatigue Behavior of a Functionally-Graded Titanium Matrix Composite]( "Fatigue Behavior of a Functionally-Graded Titanium Matrix Composite")
Fatigue Behavior of a Functionally-Graded Titanium Matrix Composite60,99 €![Effects of Prior Aging at 260 C in Argon on Inelastic Deformation Behavior of PMR-15 Polymer at 260 C: Experiment and Modeling]( "Effects of Prior Aging at 260 C in Argon on Inelastic Deformation Behavior of PMR-15 Polymer at 260 C: Experiment and Modeling")
Effects of Prior Aging at 260 C in Argon on Inelastic Deformation Behavior of PMR-15 Polymer at 260 C: Experiment and Modeling60,99 €
IM7/BMI 5250-4 with carbon fiber orientations and [0/90] were aged in air at 191-C for up to 1000 hours. The weight loss was analyzed during the aging process. Tension to failure tests were performed on both the unaged and aged specimens to establish a baseline for the Ultimate Tensile Strengths and Young's Modulus. Tension-tension cyclic load fatigue testing was conducted on the specimen to determine the effect of prior aging on the fatigue response of the composite. Cyclic strain accumulation was not influenced by prior aging, but it was influenced by the stress levels applied. Specimens lost 0.2% more weight than the [0/90] specimens from aging in air.
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Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.