Benchmark Problems Used to Assess Computational Aeroacoustics Codes
Turbofan Noise Reduction Associated With Increased Bypass Nozzle Flow
National Combustion Code Used to Study the Hydrogen Injector Design for Gas Turbines
Emissions Measured in the Exhaust of a CFM–56 Engine on a DC–8
SmaggIce 2D Version 1.8: Software Toolkit Developed for Aerodynamic Simulation Over Iced Airfoils
Piloted Flight Simulator Developed for Icing Effects Training
Subsonic Scarf Inlets Investigated
Parametric Inlet Tested in Glenn’s 10- by 10-Foot Supersonic Wind Tunnel
Wind-US 1.0 Released by NPARC Alliance
Directional Attenuation of Jet Noise With Eccentric Coannular Nozzle Investigated
Pressure Control for Low Earth Orbit Investigated
Synthetic Vortex Generator Jets Used to Control Separation on Low-Pressure Turbine Airfoils
Object-Oriented Version of Glenn-HT Code Released: Glenn-HT2000
Last updated: July 8, 2005
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