Aeroelastic and local buckling optimisation of a variable-angle-tow composite wing-box structure

The engineering aspects of automated prepreg layup: History, present and future

D. Lukaszewicz, Carwyn Ward, Kevin Potter · Composites Part B Engineering · 2011 · 698 citations

Computing, Computer Engineering, Computer Science +10

Composite Materials in Aircraft Structures

Aircraft Engineering and Aerospace Technology · 1989 · 565 citations

Engineering, Materials Science, Aerospace Structures +6

In-plane response of laminates with spatially varying fiber orientations - Variable stiffness concept

Zafer Gürdal, Reynaldo Olmedo · AIAA Journal · 1993 · 562 citations

Engineering, Materials Engineering, Materials Science +17

Variable stiffness composite panels: Effects of stiffness variation on the in-plane and buckling response

Z. Gürdal, Brian Tatting, Chauncey Wu · Composites Part A Applied Science and Manufacturing · 2007 · 519 citations

Engineering, Materials Engineering, Materials Science +16

The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes

M. W. Hyer, H.H. Lee · Composite Structures · 1991 · 419 citations

Natural Sciences, Materials Engineering, Materials Science +16