Andere Kunden interessierten sich auch für
![Effect of Hold Times on Fatigue Behavior of Nextel 720/Alumina Ceramic Matrix Composite at 1200°C in Air And in Steam Environment]( "Effect of Hold Times on Fatigue Behavior of Nextel 720/Alumina Ceramic Matrix Composite at 1200°C in Air And in Steam Environment")
Effect of Hold Times on Fatigue Behavior of Nextel 720/Alumina Ceramic Matrix Composite at 1200°C in Air And in Steam Environment63,99 €![Tension-Compression Fatigue of Hi-Nicalon/SiC Ceramic Matrix Composite at 1200 C in Air and Steam]( "Tension-Compression Fatigue of Hi-Nicalon/SiC Ceramic Matrix Composite at 1200 C in Air and Steam")
Tension-Compression Fatigue of Hi-Nicalon/SiC Ceramic Matrix Composite at 1200 C in Air and Steam63,99 €![Monotonic and Fatigue Loading Behavior of an Oxide/Oxide Ceramic Matrix Composite]( "Monotonic and Fatigue Loading Behavior of an Oxide/Oxide Ceramic Matrix Composite")
Monotonic and Fatigue Loading Behavior of an Oxide/Oxide Ceramic Matrix Composite63,99 €![Composite Materials and Processing]( "Composite Materials and Processing")
Composite Materials and Processing113,99 €![High-Temperature Matrix Cracking, Opening and Closure in Ceramic-Matrix Composites]( "High-Temperature Matrix Cracking, Opening and Closure in Ceramic-Matrix Composites")
High-Temperature Matrix Cracking, Opening and Closure in Ceramic-Matrix Composites70,99 €![Effect of Prior Aging on Fatigue Behavior of IM7/BMI 5250-4 Composite at 191-C]( "Effect of Prior Aging on Fatigue Behavior of IM7/BMI 5250-4 Composite at 191-C")
Effect of Prior Aging on Fatigue Behavior of IM7/BMI 5250-4 Composite at 191-C63,99 €![Performance of Scattering Matrix Decomposition and Color Spaces for Synthetic Aperture Radar Imagery]( "Performance of Scattering Matrix Decomposition and Color Spaces for Synthetic Aperture Radar Imagery")
Performance of Scattering Matrix Decomposition and Color Spaces for Synthetic Aperture Radar Imagery63,99 €
The aerospace community continues to push the envelope in engineering aircraft that fly higher, faster, and safer while operating with a greater degree of efficiency. To meet these operational requirements innovative aerospace components must be designed to operate in aggressive environments. The effects of creep loading history on the tensile and compressive material behavior will also be examined. The primary strengths of the N720/A composite are its oxide/oxide composition which inherently resists oxidation and a porous matrix which enables crack deflection producing enhanced matrix damage tolerance. Mechanical testing showed a significant decrease in the compressive performance of N720/A when exposed to steam environment. Conversely, N720/A specimens tested in compressive creep in air experienced an increase in compressive performance. SEM analysis showed that densification of the -alumina matrix occurred in both test environments. In air densification sinters the matrix resulting in a strengthening effect. Whereas, in steam environment analysis shows the addition of hydrogen induces hydrothermal softening of the matrix resulting in a significant loss of the compressive performance of N720/A.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.