Providence / Honolulu / Bains / San Diego / Long Beach / Edinburgh / /
Company
Firehole Composites Inc. / Autodesk Inc. / the Boeing / Firehole Technologies / Dassault Systèmes Simulia Corp. / /
Country
United Kingdom / /
Event
M&A / /
Facility
Oregon State University / I. Hyder Oregon State University / /
IndustryTerm
energy degradation parameters / energy degradation / finite element software / kinetic energy / quicker and more accurate solutions / internal energy / energy degradation values / finite element solution / large composite space structures using multicontinuum technology / quasi-static solution / explicit solution / software package / bi-linear energy law / digital signal processing / models utilizing energy degradation criteria / energy / /
NaturalFeature
Brian Bay / /
Organization
Congress / Oregon State University / Federal Aviation Authority / FAA Center of Excellence / National Aeronautics and Space Administration / Petroleum Division / American Society of Mechanical Engineers / /
Person
Gerald Mabson / Tom Walker / Larry Ilcewicz / Brian Bay / Curt Davies / Kenik / Lynn Pham / John Parmigiani / Tim Kennedy / /
Position
finite element composites model / " / representative / D.J. / composite panels representative / /
Product
Nokia N95 Smartphone / /
ProvinceOrState
New Jersey / Rhode Island / California / /
Technology
large composite space structures using multicontinuum technology / Simulation / DSP / /
Failure of Notched Laminates Under Out-of-Plane Bending, Phase VII Update 2014 JAMS Meeting J.P. Parmigiani, N. Atanasov, I. Hyder Oregon State University, Corvallis, OR, 97331 The need for understanding and predicting f