B. Farahmand

发表

Obtaining Fracture Properties by Virtual Testing and Molecular Dynamics Techniques

G. Odegard, B. Farahmand, 2009 .

Analytical Method of Generating DA/DN Curve for Aerospace Alloys

B. Farahmand, B. Farahmand, 2006 .

Fracture Properties Estimation of Aluminum Lithium Alloys Subjected to Exposure Time (Analytical Approach Versus Physical Testing)

B. Farahmand, 2004 .

Fatigue crack growth discrepancies with stress ratio

C. Rodopoulos, Rhys Jones, B. Farahmand, 2009 .

Crack Growth in Mil Annealed Ti-6AL-4V Structural Components

Rhys Jones, S. Pitt, B. Farahmand, 2012 .

Crack Healing And Crack Closure Retardation Effect Through Release of Liquid Monomer In The Wake of Crack

S. Maiti, B. Farahmand, 2009 .

An analysis approach toward FAA certification for damage tolerance of aircraft components

Frank Abdi, Kamran Nikbin, Y. Xue, 2014, The Aeronautical Journal (1968).

Observations on fatigue crack growth in a range of materials

Susan Pitt, T. Constable, B. Farahmand, 2011 .