Aging Aircraft Science and Technology Issues and Challenge and USAF Aging Aircraft Program
Electrochemical Impedance Pattern Recognition for Aircraft Hidden Chemical Corrosion Detection
Crack Initiation in Aluminum Plates With Multiple Defects
Use of Composite Patches as Reinforcements and Crack Arrestors in Aircraft Structures
Impedance Imaging for Prediction and Detection of Airframe Corrosion
Technical Considerations for Managing Aging Rotorcraft
Synergism Between Corrosion and Fatigue of AL2024-T3 Alloy
Corrosion Fatigue of Aluminum and GLARE Riveted Lap Joints
An FEAM Based Methodology for Analyzing Composite Patch Repairs of Metallic Structures