1. Assessment of composite damage growth tools for aircraft structure part I;Engelstad,2015
2. Assessment of reduced order homogenization for damage tolerant design principles (DTDP) of advanced composite aircraft structures;Shojaei,2015
3. Static validation of composite open hole analysis technique for standard and nonstandard laminate – part I;Abdi,2015
4. Application of reduced order multiscale homogenization to ’assess and quantify the benefits of applying damage tolerant design principles to advanced composite aircraft structures’;Bogdanor,2015
5. Tensile and compressive strength prediction in laminated composites by using discrete damage modeling;Iarve,2015