Structural Benchmark Tests of Composite Combustion Chamber Support Completed
Benchmark Calibration Tests Completed for Stirling Convertor Heater Head Life Assessment
Titanium Aluminide Scramjet Inlet Flap Subelement Benchmark Tested
Stainless-Steel-Foam Structures Evaluated for Fan and Rotor Blades
Integrity of Polymethylmethacrylate (PMMA) Chemically Welded Joints Examined
Life Predicted in a Probabilistic Design Space for Brittle Materials With Transient Loads
Liquid-Hydrogen-Cooled 450-hp Electric Motor Test Stand Being Developed
High-Temperature (1000 °F) Magnetic Thrust Bearing Test Rig Completed and Operational
G2 Flywheel Module Operated at 41,000 rpm
Fuel-Cell-Powered Electric Motor Drive Analyzed for a Large Airplane
Damage-Tolerant, Affordable Composite Engine Cases Designed and Fabricated
Prototype Variable-Area Exhaust Nozzle Designed
Switched-Reluctance Cryogenic Motor Tested and Upgraded
Analytical Micromechanics Modeling Technique Developed for Ceramic Matrix Composites Analysis
Design Sensitivity for a Subsonic Aircraft Predicted by Neural Network and Regression Models
Advanced Vibration Analysis Tool Developed for Robust Engine Rotor Designs
System Developed for Real-Time Blade-Flutter Monitoring in the Wind Tunnel
Flutter Stability Verified for Trailing Edge Blowing Fan
Fundamental Mistuning Model for Probabilistic Analysis Studied Experimentally
Primal and Dual Integrated Force Methods Used for Stochastic Analysis
Spur Gear Wear Investigated in Support of Space Shuttle Return-To-Flight Efforts
High-Temperature Knitted Spring Tubes Improved for Structural Seal Applications
Advanced Ceramic Wafer Seals Demonstrated at 2000 °F
Software Developed for Analyzing High-Speed Rolling-Element Bearings
Oxide Ceramic Films Grown on 60 Nitinol for NASA and Department of Defense Applications
Tribological Behavior of Nano-Onions in Krytox 143AB Evaluated
Journal Bearing Analysis Suite Released for Planetary Gear System Evaluation
Last updated: July 8, 2005
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