Titanium Dwell Fatigue

Introduction Most engineers have an intuitive feel for fatigue: apply a stress repeatedly, and eventually the material cracks — even if each individual load is well below the static yield strength. Dwell fatigue adds a further, less intuitive twist. Dwell fatigue occurs when a sustained… Read more

Strain Rate Effects: Why Metals Get Stronger but Less Ductile Under Dynamic Loading

Strain Rate Effects: Why Metals Get Stronger but Less Ductile Under Dynamic Loading Introduction A common observation in shock, impact, and ballistic engineering is that metals behave differently under dynamic loading than they do under slow, quasi-static loading. A structural steel or aluminum alloy that… Read more

The Challenge of the Ringing Moon: Structural Dynamics and Fatigue Design for Lunar Habitats

As NASA’s Artemis program and international space agencies transition from short-duration sorties to a sustained human presence on the Moon, mission planners and structural engineers must confront a mechanical hazard that received little attention during the Apollo era: lunar seismicity. The Moon is not a… Read more

Fatigue Cracks in Anodized Coatings

Image reference: https://onlinelibrary.wiley.com/doi/full/10.1002/adem.202300394 What Is Anodizing? Anodizing is widely used to improve corrosion resistance and surface durability in aluminum and other light metals. However, under cyclic loading, anodized coatings can play a surprising, and sometimes detrimental, role in fatigue performance. This post walks through why… Read more

United Airlines Flight 328

United Airlines Flight 328 was a scheduled domestic passenger flight from Denver to Honolulu, Hawaii on February 20, 2021. The Boeing 777-200 aircraft operating the route suffered engine failure shortly after takeoff The failure was “contained” but resulted in a debris field at least one… Read more

Material Shock Loading

The plot shows the applied strain on the horizontal axis and the resisting stress on the vertical axis. The area inside the triangle represents the maximum energy that can be absorbed elastically, if the member is strained up to its proportional limit stress. The member… Read more