Trailing Edge Blowing Tested for Fan Blade Wake Management
New Procedure Created for Studying Core Noise
Technique Improved for Measuring Noise Sources in Supersonic Jets Via Two-Point Space-Time Correlations
Planar Laser-Induced Fluorescence and Particle Imaging Velocimetry Used To Characterize a Baseline Nine-Point Lean Direct Injector for Comparison With National Combustor Code Results
Fuel Injector-Mixer Concepts Examined for Kerosene and Diesel Fuel Reformer Applications Using Laser-Based Techniques
Alternative Fuels Research Laboratory Being Designed and Constructed
End-to-End System Analysis Tool Developed for Studying Lunar In Situ Resource Utilization
Alternative Rotational Raman Thermometry Developed for Turbulent Combustion
Quantitative, Single-Shot, Multiscalar Measurements Demonstrated in a High-Pressure, Swirl-Stabilized Turbulent Flame
High-Throughput Triple-Grating Spectrograph Developed for Nonintrusive Measurements of Combustion-Generated Plasmas
Outer Planet Mining Vehicle Design Issues Identified and Analyzed
Aerospace Fuels Assessed for Future Aerospace Vehicles
Fuel-Injector Concepts Investigated in the Fuel-Reforming Injector Test Facility
Aerosol Microphysics in a Pressure-Reduction Chamber Predicted by Numerical Simulations
Compressor Stability Model Developed
Baseline Inlet Tests Conducted for Supersonic Inlet Flow Control in a Partial Isentropic External Compression Inlet
Wind-US Code Updated
Effect of Wedge-Shaped Deflectors on the Flow Field of a High-Bypass-Ratio Nozzle Studied
SmaggIce 2D Version 2.0: Capabilities Added for the Interactive Grid Generation of Iced Airfoils
Liquid Acquisition Devices Evaluated
Catalytic Reforming Technologies Investigated for Hydrogen Production and Onboard Aerospace Power Generation
Low-Gravity Gauging Concept Extended to Cryogenic Propellants
Liquid Oxygen-Liquid Methane Ignition Demonstrated for Application to Reaction Control Engines
Last updated: October 3, 2007
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