| Home >> Projects |
| Title | Sponsors | Dates |
|---|---|---|
| Unsteady Behavior Of A Tip - Leakage Vortex Produced By Stator - Rotor Interaction | Office of Naval Research | 3/2002 - 2/2005 |
| Predicting Modes Of The Unsteady Vorticity Field Near The Trailing Edge Of A Blade | SNASA Glenn | 1/2002 - 1/2004 |
| Blade blocking and its influence on large scale high Reynolds number turbulence convecting through a cascade of blades: Measurements | Office of Naval Research | 2/2001 - 2/2003 |
| Modeling of Unsteady Internal Flows in AeroEngines for Noise Prediction Codes | NASA (joint with Florida Atlantic University) | 1/2000 - 12/2000 |
| Aerodynamic Studies Related To The Aeroacoustics Of Tiltrotor Blades | NASA | 3/2000 - 8/2002 |
| Characterizing the Unsteady Vortical Flow Generated Downstream of the Tip of an Axial Pump Rotor Blade | Office of Naval Research | 2/1999 - 1/2002 |
| Title | Sponsors | Dates |
|---|---|---|
| The Interaction of Inflow Turbulence with a Cascade of Propulsor Blades | Office of Naval Research | 01/1999 - 01/2001 |
| Turbulence in Helicopter Rotor Flows and the Mechanism of Noise Production | NASA Langley Aeroacoustics | 1997 - 2000 |
| Tip Leakage Vortices in High Bypass Ratio Fans | NASA Langley Aeroacoustic | |
| Single Wing - Tip Vortices | Office of Naval Research NASA Langley Aeroacoustics |
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| Wake of a lifting wing | Office of Naval Research NASA Langley Aeroacoustics |
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| Studies of Complex, Equilibrium and Lifting Wakes | NASA Langley Aeroacoustics Office of Naval Research |
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| Counter - rotating tip - vortex pairs | Advanced Research Projects Agency | |
| Co - rotating tip - vortex pairs | ||
| Perpendicular Blade Vortex Interaction | NASA Langley Aeroacoustics | |
| Instrumentation development |