Technical Memorandum (TM)
September 7, 2013
June 1, 2005
Work of the US Gov. Public Use Permitted.
Available Downloads 20050228985.pdf STI
Related Records20050215680Analytic SubsidiaryGlenn's Telescience Support Center Provided Around-the-Clock Operations Support for Space Experiments on the International Space Station20050217292Analytic SubsidiaryPrototype Variable-Area Exhaust Nozzle Designed20050217241Analytic SubsidiaryStructural Benchmark Tests of Composite Combustion Chamber Support Completed20050217232Analytic SubsidiaryJournal Bearing Analysis Suite Released for Planetary Gear System Evaluation20050220636Analytic SubsidiaryOzone Exposure System Designed and Used to High-Altitude Airship Materials20050217303Analytic SubsidiaryFundamental Mistuning Model for Probabilistic Analysis Studied Experimentally20050217185Analytic SubsidiaryQuick Access Rocket Exhaust Rig Testing of Coated GRCop-84 Sheets Used to Aid Coating Selection for Reusable Launch Vehicles20050215653Analytic SubsidiaryCapillary Flow Experiments Began on the International Space Station20050217480Analytic SubsidiaryBinary Colloidal Alloy Test-3 (BCAT-3) Tabletop Space Station Experiment Continues20050217460Analytic SubsidiarySmaggIce 2D Version 1.8: Software Toolkit Developed for Aerodynamic Simulation Over Iced Airfoils20050217105Analytic SubsidiaryGlenn Refractory Adhesive for Bonding and Exterior Repair (GRABER) Developed for Repairing Shuttle Damage20050215686Analytic SubsidiaryLow-Speed Active Flow Control Laboratory Developed20050220611Analytic SubsidiaryTheoretical and Experimental Unsteady Aerodynamics Compared for a Linear Oscillating Cascade With a Supersonic Leading-Edge Locus20050217412Analytic SubsidiaryAdaptive Technologies Developed and Demonstrated for Extending the Stable Operating Range of Compressors20050215691Analytic SubsidiaryIntelligent Life-Extending Controls for Aircraft Engines Studied20050217470Analytic SubsidiaryWind-US 1.0 Released by NPARC Alliance20050217247Analytic SubsidiaryStainless-Steel-Foam Structures Evaluated for Fan and Rotor Blades20050217467Analytic SubsidiarySubsonic Scarf Inlets Investigated20050217234Analytic SubsidiaryMicrosystem Cooler Concept Developed and Being Fabricated20050217243Analytic SubsidiaryBenchmark Calibration Tests Completed for Stirling Convertor Heater Head Life Assessment20050216446Analytic SubsidiaryMolecular Rayleigh Scattering Techniques Developed for Measuring Gas Flow Velocity, Density, Temperature, and Turbulence20050215693Analytic SubsidiaryInnovative Adaptive Control Method Demonstrated for Active Suppression of Instabilities in Engine Combustors20050217255Analytic SubsidiaryLife Predicted in a Probabilistic Design Space for Brittle Materials With Transient Loads20050217027Analytic SubsidiarySonoluminescence: A Galaxy of Nanostars Created in a Beaker20050217468Analytic SubsidiaryPiloted Flight Simulator Developed for Icing Effects Training20050217163Analytic SubsidiaryFlexible Metallic Overwrap Concept Developed for On-Orbit Repair of Space Shuttle Orbiter Leading Edges20050217257Analytic SubsidiaryFuel-Cell-Powered Electric Motor Drive Analyzed for a Large Airplane20050217395Analytic SubsidiaryPower Requirements Determined for High-Power-Density Electric Motors for Electric Aircraft Propulsion20050217475Analytic SubsidiaryNew Species of Fire Discovered: Fingering Flamelets Form a Dynamic Population20050217397Analytic SubsidiaryTurbofan Noise Reduction Associated With Increased Bypass Nozzle Flow20050216445Analytic SubsidiaryNondestructive Evaluation Tests Performed on Space Shuttle Leading- Edge Materials Subjected to Impact20050217246Analytic SubsidiaryIntegrity of Polymethylmethacrylate (PMMA) Chemically Welded Joints Examined20050215694Analytic SubsidiaryDiscrete Event Supervisory Control Applied to Propulsion Systems20050217296Analytic SubsidiaryDesign Sensitivity for a Subsonic Aircraft Predicted by Neural Network and Regression Models20050217028Analytic SubsidiaryProcess Developed for Fabricating Engineered Pore Structures for High- Fuel-Utilization Solid Oxide Fuel Cells20050217250Analytic 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Tested20050217192Analytic SubsidiaryVery Tough, Erosion-Resistant Turbine Airfoil Thermal Barrier Coatings Developed20050217398Analytic SubsidiarySpur Gear Wear Investigated in Support of Space Shuttle Return-To-Flight Efforts20050217256Analytic SubsidiaryHigh-Temperature (1000 F) Magnetic Thrust Bearing Test Rig Completed and Operational20050217411Analytic SubsidiaryEmissions Measured in the Exhaust of a CFM-56 Engine on a DC-820050217394Analytic SubsidiaryAdvanced Ceramic Wafer Seals Demonstrated at 2000 deg. F20050217165Analytic SubsidiaryMechanical and Electrical Properties of a Polyimide Film Significantly Enhanced by the Addition of Single-Wall Carbon Nanotubes20050217101Analytic SubsidiaryAs-Fabricated Reinforced Carbon/Carbon Characterized20050217169Analytic SubsidiaryHigh-Temperature Piezoelectric Ceramic Developed20050217176Analytic SubsidiaryProton-Exchange-Membrane Fuel Cell Powerplants Developed and Tested for Exploration Missions20050217472Analytic SubsidiaryPressure Control for Low Earth Orbit Investigated20050217175Analytic SubsidiaryPotential High-Temperature Shape-Memory-Alloy Actuator Material Identified20050217161Analytic SubsidiaryNonhumidified High-Temperature Membranes Developed for Proton Exchange Membrane Fuel Cells20050217205Analytic SubsidiaryStirling Convertor System Dynamic Model Developed20050217179Analytic SubsidiaryProcessing of Ni30Pt20Ti50 High-Temperature Shape-Memory Alloy Into Thin Rod Demonstrated20050217404Analytic SubsidiarySoftware Developed for 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Improved by Preparation of Polyhedral Oligomeric Silsesquioxane (POSS) Nanocomposites20050217096Analytic SubsidiaryNanorod Material Developed for Use as an Optical Sensor Platform20050217295Analytic SubsidiaryAnalytical Micromechanics Modeling Technique Developed for Ceramic Matrix Composites Analysis20050215648Analytic SubsidiaryFundamental Research Applied To Enable Hardware Performance in Microgravity20050217023Analytic SubsidiaryNew Deep Reactive Ion Etching Process Developed for the Microfabrication of Silicon Carbide20050217171Analytic SubsidiaryEffects of High-Temperature Exposures on the Fatigue Life of Disk Superalloys Examined20050217408Analytic SubsidiaryTransferable Calibration Standard Developed for Quantitative Raman Scattering Diagnostics in High-Pressure Flames20050215642Analytic SubsidiaryProbabilistic Analysis Techniques Applied to Complex Spacecraft Power System Modeling20050217471Analytic SubsidiaryDirectional Attenuation of Jet Noise With Eccentric Coannular Nozzle Investigated20050217396Analytic SubsidiaryBenchmark Problems Used to Assess Computational Aeroacoustics Codes20050217473Analytic SubsidiarySynthetic Vortex Generator Jets Used to Control Separation on Low-Pressure Turbine Airfoils