AIAA-2004-4939 The NASA Dryden AAR Project: A Flight Test Approach to an Aerial Refueling System
Min-Max Formulation for Heterogeneous Composite Plates with Thermal Residual Stresses
Characterization and comparison of low energy impact damage for composite plates
Characterization and Comparison of Low Energy Impact Damage for Composite Plates
The Virtues of Multicontinuum Mechanics for Composites Analysis
The simplest rectangular finite element for plate bending analysis
The Simplest Rectangular Finite Element for Plate Bending Analysis