Sarpotdar, S. Raman, G., Sharma S., and Cain, A., “Jet Impingement Tone Suppression Using Powered Resonance Tubes,” AIAA J., Vol. 45, No. 5, May 2007.

Cain, A. B., Kerschen, E. J., Tassy, J. M. and Raman, G., “Simulation of Powered Resonance Tubes: Helmholtz Resonator Geometries,” AIAA-2004-2690.

Kerschen, E. J., Cain, A. B. and Raman, G., “Analytical Modeling of Helmholtz Based Powered Resonance Tubes”, AIAA-2004-2691.

Raman, G., Sarpotdar, S., Tassy, J., Cain, A. B. and Kerschen, E. J., “An Overview of the Development of High Bandwidth Powered Resonance Tube Actuators: Experiments and Simulations,” AIAA-2004-2856.

Raman, G., Khanafseh, S., Cain, A. B., Kerschen, E. J., “Development of High Bandwidth Powered Resonance Tube Actuators with Feedback Control,” J. Sound and Vibration, 269 (2004) pp. 1031-1062.

Cain, A. B., Kerschen, E.J., Raman, G., and Sarpotdar, S., “Simulation of Powered Resonance Tubes: Understanding Parameter Space,” AIAA-2003-3103.

Cain, A. B., Kerschen, E. J. and Raman, G., “Simulation of Acoustic characteristics and Mechanism of Powered Resonance Tubes,” AIAA-2002-2400.

Wittich, D. J., Duffin, D. A., Jumper, E. J., Cain, A. B., and Kerschen, E. J., “Passive Shear Layer Regularization Experiments in Wind Tunnels and Feed-Forward Adaptive-Optic Correction,” AIAA 2009-358, Jan. 2009.

Cain, A., Ng, T. T., Jumper, E., Wittich, D., Cavalieri, D., and Kerschen, E. “Optical Propagation Improvement System: Use of a Cavity for Regularization,” AFRL/RD invited workshop, Albuquerque, NM, Nov. 2008.

Cain, A., Ng, T. T., Jumper, E., Wittich, D., Cavalieri, D., and Kerschen, E., “An Optical Propagation Improvement System and the Importance of Aeroacoustics,” AIAA-2008-4212.

Cress, J., Gordeyev, S., Jumper, E., Ng T. T., and Cain, A., “Similarities and Differences in Aero-Optical Structure over Cylindrical and Hemispherical Turrets with a Flat Window,” AIAA-2007-0326.

Gordeyev, S., Jumper, E. J., Ng, T. T. and Cain, A. B., “Optical Disturbances Caused by Transonic Separated Boundary Layers Behind a 20-Degree Ramp: Physics and Control,” AIAA-2004-0472.

Gordeyev, S., Jumper, E. J., Ng, T. T. and Cain, A. B., “Aero-Optical Characteristics of Compressible, Subsonic Turbulent Boundary Layers,” AIAA-2003-3606.

C. Nelson, A. Cain, E. Kerschen and G. Raman, “Simulations of Helmholtz Resonator Powered Resonance Tubes at Moderate Pressure Ratios,” AIAA-2008-0800.

Kerschen, E. and Cain A. , “Aeroacoustic Mode Trapping for a Wind Tunnel with a Cavity in the Wall,” AIAA-2008-4213.

Cain, A., Ng, T. T., Jumper, E., Wittich, D., Cavalieri D., and Kerschen, E., “An Optical Propagation Improvement System and the Importance of Aeroacoustics,” AIAA-2008-4212.

Sarpotdar, S. Raman, G., Sharma S., and Cain, A. “Jet Impingement Tone Suppression Using Powered Resonance Tubes,” AIAA J., Vol. 45, No. 5, May 2007.

Lopera, J., Ng, T. T., and Cain, A., “Experimental Studies on Jet Mixing and Noise Control utilizing Vortex Shedding Pins and Moderately Lobed Nozzles,” AIAA-2006-0312.

Raman, G. and Cain, A. B. “Innovative actuators for active flow and noise control,” Proc. Instn. Mech. Engrs. (2002) Vol. 216 Part G: J. Aerospace Engineering, pp 303-324.

Bortz, D.M., Rubio, A. D., Banks, H. T., Cain, A. B., and Smith, R. C., “ Control of open bay acoustics by harmonic mass injection,” International J. of Aeroacoustics, Vol. 1, Num. 1, pp. 65-82, 2002.

Cain, A. B., Rubio, A. D., Bortz, D. M., Banks, H. T., and Smith, R. C. "Optimizing Control of Open Bay Acoustics," AIAA 2000-1928.

Raman, G., Kibens, V, Cain, A. , and Lepicovsky, “Advanced Actuator Concepts for Active Aeroacoustics Control,” AIAA 2000-1930.

Nelson, C. C., Invited participant at 2005 NPARC Alliance Workshop, Feb. 2005, Arnold Air Force Base, TN.

Patel, M. P., Carver, R. and Cain, A. B., “CFD studies on Flow Through Nozzles Using Wind-US at Low Mach Numbers,” AIAA Paper 2004-0531.

Patel, M. P., Ng, T. T. and Cain, A. B., “A CFD Study of a Missile Aero Control Fin by Near-Wall Flow Modifications,” AIAA 2003-0547.

Patel, M. P. and Cain, A. B., “Numerical Simulation of Flow Control Techniques for Separation Control,” AIAA 2002-0668.

Patel, M. P. and Cain, A. B., “Computational Studies of Active Control of Boundary Layer Separation,” ASME Piping and Pressure Vessels Meeting, Atlanta , GA , July, 2001.

Smith, T. D., Cain, A. B. , and Chenault, L. F. , “Numerical Simulation of Enhanced Mixing in Jet Plumes Using Pulsed Blowing,” J. of Aircraft, June 2001, V38, No. 3, pp. 458-463.

Smith, T. D., Cain, A. B. , and Chenault, L. F. , “Numerical Simulation of Enhanced Mixing in Jet Plumes Using Pulsed Blowing,” ISABE-163-3, Italy , September 1999.

Schmidt, R. N. and Patel, M. P., “Aerionics – a New Aero Industry for Flight Control,” SAE International, 07ATC-159, AeroTech Congress & Exhibition, Sept 2007.

Patel, M. P., Kolacinski, R. M., Ng, T. T., and Patil, S.K.R., “Distributed Mechanical Actuators for Design of a Closed-Loop Flow-Control System,” AIAA Paper 2006-3158.

Patel, M. P., Kolacinski, R. M., Prince, T. S., Ng, T. T., and Myatt, J. H., “Novel Hierarchical Modular Control Methodology for Closed-Loop Flow-Control Applications,” J. of Aircraft, Vol. 42, No. 5, Sept-Oct 2005, pp. 1099-1108.

Patel, M. P., Tilmann, C. P., and Ng, T. T., “Active Transparent Stall Control System for Air Vehicles,” J. of Aircraft, Vol. 40, No. 5, September-October 2003.

Patel, M. P., DiCocco, J. M., Prince, T. S., and Ng, T. T., “Flow Control Using Reconfigurable Porosity,” AIAA Paper 2003-3665.

Patel, M. P., Skebe G., Ng, T. T., and Lisy, F. J., “Development of a MEMS Based Microvalve for Flow Control Using Active Dimples, AIAA 2002-0272.

Patel, M. P., Reshotko, E., and Hyman, D., “Microfabricated Shear Stress Sensors, Part-III: Reducing Calibration Uncertainty,” AIAA J., August 2002, Vol. 40, No. 8, pp. 1582-1588.

He, C., Corke, T. C., and Patel, M. P., “Plasma Flaps and Slats: An Application of Weakly-Ionized Plasma Actuators,” J. of Aircraft, Vol. 46, No. 3, pp. 864-873, May-June 2009; also AIAA Paper 2004-2127.

Nelson, R. C., Corke, T. C. and Patel, M. P., “A Smart Wind Turbine Blade Using Distributed Plasma Actuators for Improved Performance, AIAA Paper 2008-1312, Jan 2008.

Patel, M. P., Ng, T. T., Vasudevan, S., Santavicca, E., Corke, T. C., Post, M., McLaughlin, T. E., and Suchomel, C., “Scaling Effects of an Aerodynamic Plasma Actuator,” J. of Aircraft, Vol. 45, No. 1, pp. 223-236, Jan-Feb 2008.  also AIAA Paper 2007-0635.

Lopera, J., Ng, T. T., Patel, M. P., Vasudevan, S., Santavicca, E., and Corke, T. C., “Aerodynamic Control Using Windward Surface Plasma Actuators on a Separation Ramp,” J. of Aircraft, Vol. 44, No. 6, pp. 1889-1895, Nov-Dec 2007.

Patel, M. P., Ng, T. T., Vasudevan, S., Corke, T. C., and He, C., “Plasma Actuators for Hingeless Aerodynamic Control of an Unmanned Air Vehicle,” J. of Aircraft, Vol. 44, No. 4, pp. 1264-1274, July-Aug 2007.

Patel, M. P., Sowle, Z. H., Corke, T. C., and He, C., “Autonomous Sensing and Control of Wing Stall Using a Smart Plasma Slat,” J. of Aircraft, Vol. 44, No. 2, pp. 516-527, March-April 2007.

Nelson, C. C., Cain, A. B., Patel, M. P., and Corke, T. C., “A Simplified Strategy for Optimizing Flow-Control-Configured Airfoil,” AIAA Paper 2007-4274, June 25-28, 2007.

Corke, T. C., Hertz, B., and Patel, M. P., “Plasma Flow Control Optimized Airfoil,” AIAA Paper 2006-1208.

Nelson, C., Cain, A., Patel M. P., and Corke, T. , “Simulation of Plasma Actuators Using the Wind-US Code,” AIAA-2006-0634.

Corke, T. C., Tillotson, D., Patel, M. P., Su, W., and Toledo, W., “Radius Flow Vectoring for Projectile Drag and Steering Control Using Plasma Actuators,” AIAA Paper 2008-3769.

Patil, S. K. R., Ng, T. T., and Patel, M. P., “Trajectory Control of a Small Caliber Projectile Using Active Transpiration,” AIAA Paper 2007-3811.

Lopera, J., Ng, T. T., Patel, M. P., and Vasudevan, S., “Coning Motion Control of a Blunt-Nose Projectile Using Small Deployable Strakes,” AIAA Paper 2007-3812.

Lopera, J., Ng, T. T., Patel, M. P., and Vasudevan, S., “Forebody Geometry Effects on the Flow of a Blunt-Nose Projectile at High Alpha,” J. of Aircraft, Vol. 44, No. 6, pp. 1906-1922, Nov-Dec 2007.

Patel, M. P., Sowle, Z. H., Ng, T. T., and Toledo, W., “Range and Endgame Performance Assessment of a Smart Projectile Using Hingeless Flight Control,” AIAA Paper 2006-0671.

Patel, M. P., Sowle, Z. H., Stucke, R., and Ng, T. T., “Aerodynamic Control of a Small Projectile,” AIAA Paper 2006-0667.

Patel, M. P., Sowle, Z. H., Ng, T. T., and Toledo, W., “Hingeless Flight Control System of a Smart Projectile Using Miniature Actuators,” AIAA Paper 2005-5258.

Patel, M. P., Tilmann, C. P., and Ng, T. T., “Closed Loop Missile Yaw Control Via Manipulation of Forebody Flow Asymmetries,” J. of Spacecraft and Rockets, Vol. 41, No. 3, pp. 436-443, May-June 2004. (AIAA-YP Best Paper award).

Patel, M. P., DiCocco, J. M., Lopera, J., and Ng, T. T., “Active Boattailing and Aerodynamic Control Fins for Maneuvering Weapons,” AIAA Paper 2004-2696.

Patel, M. P., DiCocco, J. M., Prince, T. S., and Ng, T. T., “Afterbody Flow Control for Low-Alpha Missile Maneuvering,” AIAA Paper 2003-3673.

Nelson, C. C. and Cain, A. B., "Prediction of Store Trajectory Response to Unsteady Aerodynamic Loads," AIAA 2009-548.  Invited paper. ASM Meeting, Jan. 2009.

Cain, A., Ng, T., Jumper, E., Wittich, D., Cavalieri, D., and Kerschen, E., “Optical Propagation Improvement System: Use of a Cavity for Regularization,” AFRL/RD invited workshop, Albuquerque, NM, Nov. 2008.

Patel, M. P., “On the Use of Flow Control for Projectile Steering,” AIAA Young Professional Student Education Conference, Baltimore, MD, Nov. 10, 2006.

Patel, M. P., “Missile Maneuvering and Endgame Enhancement Using Active Flow Control,” Missiles and Munitions Industry Meeting, AMRDEC, Redstone Arsenal, Aug. 16, 2006.

A. Cain, “Observations on Optical Aberrations: Flow Control Devices and Scaling,” AFRL/DE Workshop on Directed Energy, Albuquerque, NM, Oct. 2005.

Nelson, C. C., Invited participant at 2005 NPARC Alliance Workshop, Feb. 2005, Arnold Air Force Base, TN.

Patel, M. P., Kolacinski, R. M., Prince, T. S., Ng, T. T., and Cain, A. B., “Closed-Loop Flow Control for Aircraft and Missiles,” Collaborative Center of Control Science (CCCS), The Ohio State University, Nov. 7-8, 2002.