Publications

Computational Fluid Dynamics

Harrison, N., Anderson, J., Fleming, J., Ng, W., Computational Investigation of Active Flow Control of a Boundary Layer Ingesting Serpentine Diffuser, 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2006-874, January 2006, Reno, Nevada.

Wind Tunnel Testing

Turbomachinery:

Anderson, J., Ng, W., Fleming, J., A Technique to Estimate Flow Distortion in Boundary Layer Ingesting Serpentine Inlets Using Unsteady Wall-Pressures, 45th AIAA Aerospace Sciences Meeting and Exhibit, January 2007, Reno, Nevada.

Bailie, T., Carter C., Feng, J., Ng, W., Burdisso, R., Copenhaver, W., Wake-Filling and Reduction of Rotor HCF Using Stator Trailing Edge Blowing, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 17-19, 2000, Huntsville, Alabama.

Bailie, T., Ng, W., Burdisso, R., Copenhaver, W., Blackwell, C., Reduction of Transonic Rotor Vibration Using Stator Trailing Edge Blowing, 6th National Turbine Engine High Cycle Fatigue Conference, March 5-8, 2001, Jacksonville, Florida.

Langford, M., Guillot, S., Ng, W., Breeze-Stringfellow, A., Solomon, W., and Estevadeordal, J., Experimental Investigation of the Effects of a Moving Shock Wave on Compressor Stator Flow, GT2005-68722, ASME Turbo Expo, 2005 June, Reno, NV.

Langford, M., Breeze-Stringfellow, A., Guillot, S., Solomon, W., Ng, W., and Estevadeordal, J., “Experimental Investigation of the Effects of a Moving Shock Wave on Compressor Stator Flow”, ASME Journal of Turbomachinery, Vol. 129, pp. 127-135.

Rabe, A., Ng, W., Burdisso, R., Effectiveness of a Serpentine Inlet Duct Flow Control Technique at Design and off-Design Simulated Flight Conditions, ASME Turbo Expo 2004: Power for Land, Sea, and Air, GT2004-53475, June 14-17, 2004, Vienna, Austria.

Scribben, A., Ng, W., Burdisso, R., “Effectiveness of a Serpentine Inlet Duct Flow Control Technique at Design and off-Design Simulated Flight Conditions,” ASME Journal of Turbomachinery, Vol. 128, Issue 2, pp. 332-339, April 2006.

Flow Control:

Anderson, J., Burdisso, R., Ng, W., An Active Flow Distortion Control System for Serpentine Inlets, International Mechanical Engineering Congress and Exposition, IMECE2002-NCA-33049, November 17-22, 2002, New Orleans, Louisiana.

Anderson, J., Burdisso, R., Ng, W., Rabe, A., Ölçmen, S., A Facility For Active Flow Control Research In Serpentine Inlets, 40th Aerospace Science Meeting and Exhibit, AIAA-2002-0510, January 14-17, 2002, Reno, Nevada.

Feng, N., Rao, N., Burdisso R., Ng, W., Active Flow Control Using MEMS Actuators to Reduce Fan Noise, 137th Meeting of the Acoustical Society of America and the 2nd Convention of the European Acoustics Association ASA/EAA, March 14-19, 1999, Berlin, Germany. (Invited presentation)

Halasz, C., Arntz, D., Burdisso, R., and Ng, W., “Fan Flow Control for Noise Reduction Part 1: Advanced Trailing Edge Blowing Concepts,” AIAA-2005-3025, AIAA/CEAS Aeroacoustics Conference, 2005 May, Monterey, CA.

Harrison, N., Anderson, J., Fleming, J., Ng, W., Experimental Investigation of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser, 45th AIAA Aerospace Sciences Meeting and Exhibit, January 2007, Reno, Nevada.

Langford, M., Minton, C., Ng, W., Estevadeordal, J., and Burdisso, R., Fan Flow Control for Noise Reduction Part 2: Investigation of Wake-Filling Techniques, AIAA-2005-3026, AIAA/CEAS Aeroacoustics Conference, 2005 May, Monterey, CA.

Langford, M., Minton, C., Ng, W., Burdisso, R., and Halasz, C., Fan Flow Control for Noise Reduction Part 3: Rig Testing of Optimal Design, AIAA-2005-3027, AIAA/CEAS Aeroacoustics Conference, 2005 May, Monterey, CA.

Ng, W., Burdisso, R., “MEMS and Active Flow Control for Aeropropulsion”, von Karman Institute Lecture Series, Ohio Aerospace Institute, Ohio, March 10-14, 2003.

Acoustics & Sensing:

Anderson, J., Ng, W., Burdisso, R., Truax, P., Miller, D., Niestroy, M., A Non-intrusive Sensing Technique to infer Optimal Flow Control in Serpentine Inlets, 44th AIAA Aerospace Sciences Meeting, AIAA-2006-0013, January 2006, Reno Nevada.

Anderson, J., Bailie, S., Ng, W., Acoustic Sensing of Rotor Blade Vibrations for Monitoring High Cycle Fatigue in Gas Turbine Engines, Propulsion-Safety and Affordable Readiness Program Review, March 2006, Jacksonville, Florida.

Anderson, J., Bailie, S., Ng, W., Acoustic Monitoring of Axial Compressor Rotor Blade Vibrations, AIAA/CEAS Aeroacoustics Conference, AIAA-2006-2577, May 2006, Cambridge, Massachusetts.

Fleming, J., Olcmen, S., Li, S., Burdisso, R., Ng, W., Sensing for Active Flow Control in Advanced Propulsion-Airframe Integration Systems, 42nd AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2004-1200, January 2004, Reno, Nevada.

Ng, W., Burdisso, R., Active Acoustic and Flow Control for Aeropropulsion, 39th AIAA Aerospace Sciences Meeting & Exhibit, AIAA-2001-0220, January 8-11, 2001, Reno, Nevada.