Reverse engineering material processing conditions through inverse prediction using particle shape analysis.
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Investigation of combined effects of radiation and vacuum on structural materials for nuclear space- craft components - materials science
Measured effects of various combinations of nuclear radiation, vacuum, and cryotemperatures on component parts of nuclear-powered spacecraft
Weight changes of solids in high vacuum and high temperature environmental simulation
Vacuum effects on liquid and semi-solid materials for space environment
Rate and extent of weight loss of 62 solid materials in vacuum environment
Vacuum and nuclear radiation effect on space vehicle and powerplant organic materials, emphasizing accessory hardware
Thermal diffusivity measurement, thermoelectric properties of graphite alloys and compounds, superconductivity in tungsten films, and gas pump based on thermal transpiration
S-13G type thermal control coatings for space applications
Thermal diffusivity, energy storage devices, thermoelectricity in graphite alloys, superconductivity in tungsten films, and thermionic converter
Recent activities of the Lewis Research Center are reviewed which are directed toward developing materials for rotating hot section components for aircraft gas turbines. Turbine blade materials activities are directed at increasing metal temperatures approximately 100 C compared to current directionally solidified alloys by use of oxide dispersion strengthening or tungsten alloy wire reinforcement of nickel or iron base superalloys. The application of thermal barrier coatings offers a promise of increasing gas temperatures an additional 100 C with current cooling technology. For turbine disk alloys, activities are directed toward reducing the cost of turbine disks by 50 percent through near net shape fabrication of prealloyed powders as well as towards improved performance. In addition, advanced alloy concepts and fabrication methods for dual alloy disks are being studied as having potential for improving the life of future high performance disks and reducing the amount of strategic materials required in these components.
Program incorporates non-Rayleigh effects in evaluating structure life. RMS2 computer program converts constant amplitude fatigue allowables to random-loading allowables, with influence of peak distribution and mean stress considered. RMS2 written in FORTRAN IV.
High temperature environmental attack of dollar intensive turbine components reduces turbine efficiency and can limit life. The mechanisms of alloy and coating attack and the effects of interaction with the environment on mechanical behavior. This base of understanding provides the foundation for developing life prediction methods and identifying strategies for controlling attack. Subjects discussed in detail include oxidation and new developments in thermal barrier coating research.
Using the George Washington University biaxial test system, a static fracture toughness study of two polymers (PMMA and PVC) and three aluminum alloys was performed for several variations in specimen geometry. Photoelastic experiments indicate that the applied load biaxiality has a very strong influence on the size and shape of the crack-tip stress field, and fracture toughness values for both polymers were seen to decrease with increasing load biaxiality. The load biaxiality was also found to have a strong influence on the crack growth direction in PMMA and a negligible influence on the PVC. The 7075-T6 aluminum toughness values increased with biaxiality, while intermediate peak toughness values were noted at a 0.5 biaxiality ratio for the more ductile 2024-T3 and 6061-T4 alloys. Fracture toughnesses at the highest biaxiality ratios were found to be equal to the uniaxial results.