Evolution of USAF Damage Tolerance design philosophy

In the early days of aviation, the concept of fatigue life was not a prime consideration in design. Aircraft did not typically have a long service life and were designed based on ultimate strength. Early aircraft failures occurred due to component/system failures, combat damage, and pilot error. Aircraft did not typically last long enough for fatigue to become an issue. As the design of aircraft became more sophisticated and pilot skill increased, aircraft began to last longer and fatigue became a critical concern. Continue reading Evolution of USAF Damage Tolerance design philosophy

Failure analysis of high strength nuts

Fracture and fatigue are important material performance issues that Hill Engineering examines on a regular basis. Hill Engineering recently contributed to a publication titled “Investigating and interpreting failure analysis of high strength nuts made from nickel-base superalloy.” The publication includes a detailed review of work performed to understand the failure of these fracture critical nuts. The abstract text is copied below. A temporary link to download a pdf of the publication is provided at the bottom. Continue reading Failure analysis of high strength nuts