NASA Armstrong's Structural Dynamics Testing Capabilities and Testing Facility
F/A-18 Strain Gage Loads Calibration Test
Test and Simulation of a Fokker F28 Crash Landing
Vibro-Acoustic Test Article (VATA) Test Series
DIAMOND - An Architecture for Persistent Space Platforms
Substructure Versus Property-Level Dispersed Modes Calculation
Shell Buckling Knockdown Factor Project Overview and Status
ISS Inspection Capabilities and Challenges
Shape Sensing for Wings with Spars and Ribs Using Simulated Strain
Full-Scale Crash Testing of Transport Rotorcraft
AMTD -Advanced Mirror Technology Development in Mechanical Stability
PAT Wing Fixed Base Correction Modal Testing Debrief
Future Applications of Lightweight Expandable Structures for NASA Space Science
3-Dimenstional Multifunctional Ablative Thermal Protection System (3D-MAT) Invention Overview
Structural Design and Aeromechanical Analysis of Unconventional Blades for Future Mars Rotorcraft
X-Plane Structures Challenges Lessons Learned
The Mission Loads Environment and Structural Design of the Mars Science Laboratory Spacecraft