Nicht lieferbar
Andere Kunden interessierten sich auch für
![Fretting Fatigue Behavior of a Titanium Alloy Ti-6AL-4V at Elevated Temperature]( "Fretting Fatigue Behavior of a Titanium Alloy Ti-6AL-4V at Elevated Temperature")
Fretting Fatigue Behavior of a Titanium Alloy Ti-6AL-4V at Elevated Temperature52,99 €![Fretting Fatigue Behavior of Nickel Alloy IN-100]( "Fretting Fatigue Behavior of Nickel Alloy IN-100")
Fretting Fatigue Behavior of Nickel Alloy IN-10052,99 €![Biaxial Fatigue Behavior of Niti Shape Memory Alloy]( "Biaxial Fatigue Behavior of Niti Shape Memory Alloy")
Biaxial Fatigue Behavior of Niti Shape Memory Alloy52,99 €![Behavior of Three Metallic Alloys under Combined Axial-Shear Stress at 650 C]( "Behavior of Three Metallic Alloys under Combined Axial-Shear Stress at 650 C")
Behavior of Three Metallic Alloys under Combined Axial-Shear Stress at 650 C53,99 €![Analysis of Methods for Determining High Cycle Fatigue Strength of aA Material with Investigation of Ti-6Al-4V Gigacycle Fatigue Behavior]( "Analysis of Methods for Determining High Cycle Fatigue Strength of aA Material with Investigation of Ti-6Al-4V Gigacycle Fatigue Behavior")
Analysis of Methods for Determining High Cycle Fatigue Strength of aA Material with Investigation of Ti-6Al-4V Gigacycle Fatigue Behavior52,99 €![Fatigue Behavior of a SiC/SiC Composite at 1000°C in Air and Steam]( "Fatigue Behavior of a SiC/SiC Composite at 1000°C in Air and Steam")
Fatigue Behavior of a SiC/SiC Composite at 1000°C in Air and Steam53,99 €
Fretting fatigue is the surface damage that occurs at the interface between two components that are undergoing a small amplitude oscillatory movements. It results in a reduction of the material life as compared to the plain fatigue. Most of the previous works were accomplished under a constant applied normal load and a little effort was done under a variable contact load, while none of these studies has considered the phase difference between the axial load and the contact load. The primary goal of this study is to investigate the effect of phase difference between axial and contact loads on fretting fatigue behavior of Ti-6Al-4V alloy. The frequency of both axial and contact loads was the same. i.e. 10 Hz. Under variable contact load condition; only the axial stress range and the phase angle were varied. This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.