Characterization and Comparison of Low Energy Impact Damage for Composite Plates
The simplest rectangular finite element for plate bending analysis
The Simplest Rectangular Finite Element for Plate Bending Analysis
Impact of Dynamics on the Design of the RL10B-2 Extendible Carbon-Carbon Exit Cone
Min-Max Formulation for Heterogeneous Composite Plates with Thermal Residual Stresses
AIAA-2004-4939 The NASA Dryden AAR Project: A Flight Test Approach to an Aerial Refueling System