NASA NTRS · 20010019405
Simple Elasticity Modeling and Failure Prediction for Composite Flexbeams
Abstract
A simple 2D boundary element analysis, suitable for developing cost effective models for tapered composite laminates, is presented. Constant stress and displacement elements are used. Closed-form fundamental solutions are derived. Numerical results are provided for several configurations to illustrate the accuracy of the model.
Keep this discovery
Explore connections, maps & timelines
Makeev, Andrew, Armanios, Erian, OBrien, T. Kevin. 2001-01-01. Simple Elasticity Modeling and Failure Prediction for Composite Flexbeams. https://ntrs.nasa.gov/citations/20010019405
Cite the original work for its findings. Save a collection to share your selection of sources.