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
Impact of Dynamics on the Design of the RL10B-2 Extendible Carbon-Carbon Exit Cone
The Simplest Rectangular Finite Element for Plate Bending Analysis
Characterization and Comparison of Low Energy Impact Damage for Composite Plates