Search | Fracture and Structural Integrity

Miscellanea Views: 1,692 Downloads: 513 Vol. 9, No. 34 (2015) September 29, 2015

Biaxial fatigue behavior of a powder metallurgical TRIP steel

S. Ackermann, T. Lippmann, D. Kulawinski, S. Henkel, H. Biermann

Multiaxial fatigue behavior is an important topic in critical structural components. In the present study the biaxial-planar fatigue behavior of a powder metallurgical TRIP steel (Transformation Induced Plasticity) was studied by taking…

10.3221/IGF-ESIS.34.64

Details: Biaxial fatigue behavior of a powder metallurgical TRIP steel PDF

PDF

SI: Russian mechanics contributions for Structural Integrity Views: 203 Downloads: 145 Vol. 20, No. 77 (2026) April 3, 2026 pp. 13-26

Effect of continuous carbon fiber layup architecture on tensile performance of hybrid FDM composites

Evgeniy Lobov, Mikhail Tashkinov

Hybrid continuous fiber–reinforced composites produced by fused deposition modeling (FDM) offer a promising solution for lightweight load-bearing structures. However, their mechanical performance is strongly governed by internal…

10.3221/IGF-ESIS.77.02

Details: Effect of continuous carbon fiber layup architecture on tensile performance of hybrid FDM composites PDF HTML Visual Abstract

Other formats

PDF HTML Visual Abstract Graphical Abstract Podcast

Miscellanea Views: 1,498 Downloads: 553 Vol. 7, No. 26 (2013) September 25, 2013 pp. Pages 104-122

Crack of a helicopter main rotor actuator attachment: failure analysis and lessons learned

L. Allegrucci, F. De Paolis, A. Coletta, M. Bernabei

A Light Utility Helicopter (LUH), in the course of a training flight, leaving the ground during the taxi to take off, went into an uncontrolled rolling to the right; consequently the helicopter gradually laid down on the right side. The…

10.3221/IGF-ESIS.26.11

Details: Crack of a helicopter main rotor actuator attachment: failure analysis and lessons learned PDF

PDF

Search the articles

Search results

Biaxial fatigue behavior of a powder metallurgical TRIP steel

Effect of continuous carbon fiber layup architecture on tensile performance of hybrid FDM composites

Crack of a helicopter main rotor actuator attachment: failure analysis and lessons learned