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Insitu Lunar Launch & Landing Pad Construction w/ Regolith and Thermoset Polymers
Statistical Problems in the Size Effect on Material Strength
Statistically Isotropic Deformation of Composite Materials
Thermal Protection Systems: Past, Present and Future
Development of Textile Reinforced Composites for Aircraft Structures
Inspection for Damage to Carbon/Epoxy Composite Overwrapped Pressure Vessels
Compressive Strength Properties of Fiberglass Laminates
The Potentials of Composite Structures in the Design of Aircraft
Investigating the Constraint Effect in a Particulate Composite Material
Structural Health Monitoring of a Bonded Composite Patch Repair on a Fatigue-Cracked F-111C Wing
Design Criteria and Concepts for Fibrous Composite Structures Final Report
Design and Fabrication of Full Scale Prototype Truck Chassis. Volume 1. Wheels
Implementation Guidelines for ANSI/AIAA S-081: Space Systems Composite Overwrapped Pressure Vessels
NASA Automated Fiber Placement Capabilities: Similar Systems, Complementary Purposes
The 29TH Meeting of the Structures and Materials Panel - Summary Record
Applications and Optimizations of Structural Composites for Aircraft Wings
HSCT Airframe Materials: The Boeing Perspective
Materials for Fighter Aircraft
Processing of Alumina-Toughened Zirconia Composites
Fabrication and Testing of the Composite Materials Aircraft Wing Section
Helicopter Fatigue Design Guide
Stiffness of Asphalt Cements Evaluated by Compression
Qualification of Elastic Memory Composite Hinges for Spaceflight Applications
Evaluation of Composite Wing for XFV-12A Airplane. Appendix C
Subcritical Crack Growth in a Composite Solid Propellant
Resin Transfer Molding for Advanced Composite Primary Wing and Fuselage Structures
Development of a Composite Tailoring Technique for Airplane Wing
Defense Primer: Ground Based Strategic Deterrent (GBSD) Capabilities
Reflective Crack Mitigation Guide for Flexible Pavements, Tech Transfer Summaries
Air Craft Landing Gear Brake Friction Materials Development
Aeroservoelastic Optimization of Aircraft Wings with Load Alleviation Systems
Helicopter Fatigue Life Assessment
NASA-UVA Light Aerospace Alloy and Structures Technology Program (La2st)
Modeling of Shear Thickening Fluids for Analysis of Energy Absorption Under Impulse Loading
Active Aeroelastic Tailoring of High-Aspect-Ratio Composite Wings