Single-Stage 3.4:1-Pressure-Ratio Aspirated Fan Developed and Demonstrated
Pulsed Ejector Thrust Amplification Tested and Modeled
Glow Discharge Plasma Demonstrated for Separation Control in the Low-Pressure Turbine
TopMaker: Technique Developed for Automatic Multiblock Topology Generation Using the Medial Axis
Supersonic Rocket Thruster Flow Predicted by Numerical Simulation
ThermoBuild: Online Method Made Available for Accessing NASA Glenn Thermodynamic Data
Low-Cost, User-Friendly, Rapid Analysis of Dynamic Data (RADD) System Established
Contact Angle Influence on Geysering Jets in Microgravity Investigated
Cryogenic Nitrogen Thermosyphon Developed and Characterized
Last updated: August 12, 2004
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