The effect of local dents on the residual ultimate strength of 2024-T3 aluminum alloy plate used in aircraft under axial tension tests

Modelling of Bird Strike on an Aircraft Wing Leading Edge Made from Fibre Metal Laminates – Part 2: Modelling of Impact with SPH Bird Model

M.A. McCarthy, Jing Xiao, C.T. McCarthy et al. · Applied Composite Materials · 2004 · 178 citations

Wing Design, Engineering, Impact (Mechanics) +10

Ultimate strength of cracked plate elements under axial compression or tension

Jeom Kee Paik, Yakshansh Kumar, Jae‐Myung Lee · Thin-Walled Structures · 2004 · 128 citations

Cracked Plate Elements, Structural Integrity, Engineering +11

Prediction of fatigue performance in gas turbine blades after foreign object damage

D. Nowell · International Journal of Fatigue · 2003 · 118 citations

Damage Mechanism, Engineering, Service Life Prediction +12

SPH – Lagrangian study of bird impact on leading edge wing

Michele Guida, Francesco Marulo, Michele Meo et al. · Composite Structures · 2010 · 100 citations

Wing Design, Edge Wing, Engineering +6

Ultimate strength of perforated steel plates under combined biaxial compression and edge shear loads

Jeom Kee Paik · Thin-Walled Structures · 2007 · 77 citations

Ultimate Strength, Engineering, Strength Property +9