Refereed Publications

• Alvi, F. S., Strykowski, P. J. Krothapalli, A. and Forliti, D. J. “Vectoring Thrust in Multiaxes Using Confined Shear Layers,” ,” ASME Journal of Fluids Engineering, Vol. 122, March 2000, pp. 3-13.
• Krothapalli, A., Rajakuperan, E. Alvi, F. S. and Lourenco, L., “Flow field and Noise Characteristics of a Supersonic Impinging Jet,” Journal of Fluid Mechanics, Vol. 392, August 1999, pp. 155-181.
• Shih, C., Alvi, F. S., and Washington, D., "Effects of Counterflow on the Aeroacoustic Properties of a Supersonic Jet," AIAA Journal of Aircraft, March/April1999.
• Alvi, F. S. and Strykowski, P. J. “Forward Flight Effects on Counterflow Thrust Vector Control of a Supersonic Jet,” AIAA Journal, Vol. 37, No. 2, Feb 1999.
• Alvi, F. S., Krothapalli, A., Washington D., and King, C. J. “Aeroacoustic Properties of a Supersonic Diamond-Shaped Jet,” AIAA Journal, Vol. 34, No. 8, August 1996, pp. 1562-1569.  Also presented at the 1st Joint CEAS/AIAA Aeroacoustics Conference, Munich, Germany, CEAS/AIAA Paper 95-170.
• Washington D., Alvi, F. S., Strykowski, P. J. and Krothapalli, A.,  “Multi-Axis Fluidic Thrust Vectoring of a Supersonic Jet using Counterflow,”AIAA Journal, Vol. 34, No. 8, August 1996, pp. 1734-1736.
• Alvi, F. S., Krothapalli, A. and Washington D.,  “Experimental Study of a Compressible Countercurrent Turbulent Shear Layer,” AIAA Journal. Vol. 34, No. 4, April 1996, pp. 728-735.
• Strykowski, P. J., Alvi, F. S. and Krothapalli, A., “The Role of Velocity Ratio on Supersonic Jet Mixing,” (Invited paper) 1st Joint ASME/JSME Fluids Engineering and Laser Anemometry Conference, Forum on High Speed Jet Flows, FED Vol. 214, August 1995, pp. 97-102.
• Alvi, F. S. and Settles, G. S., "Physical Model of the Swept Shock Wave/Boundary-Layer Interaction Flowfield," AIAA Paper 91-1768,  AIAA Journal., Vol. 30, No. 9, Sept. 1992, pp. 2252--2258.
• Settles, G. S.,  Alvi, F. S. and Hsu, J. C., "On the Shock Bifurcation/Jet-Impingement Structure of Swept Interactions and Related Flowfields," IUTAM Symposium on Separated Flows and Jets, Novosibirsk, Russia, 1990, edited by Kozolov, V. V. and Dovgal, A. V., Springer-Verlag, Berlin-Heidelberg, 1991, pp. 255-262.
• Kim, K. S., Lee, Y., Alvi, F. S., Settles, G. S., and Horstman, C. C., "Skin-Friction Measurements and Computational Comparison of Swept Shock/Boundary-Layer Interactions, AIAA Journal, Vol 29, No. 10, October 1991, pp.1643-1650.

Articles & Abstracts Published in Conference Proceedings

• Phalnikar, K. and Alvi, F. S., "Properties of Free and Impinging Supersonic Microjets," to be presented at the 31st AIAA Fluid Dynamics Conference and Exhibit, 11 - 14, Jun 2001, Anaheim, California.
• Alvi, F. S., Shih, C. and Krothapalli, A., “Active Control of the Feedback Loop in High Speed Jets,” AIAA Paper 2001-0373, 39th AIAA Aerospace Sciences Meeting, Reno, Jan. 2001.
• Alvi, F. S., Garg, G., Shih, C. and Krothapalli, A., “A New Approach for Controlling Unsteady Supersonic Impinging Jets," Recent Advances in Fluid Mechanics, December, 2000, Indian Institute of Science, Kanpur, India.
• Alvi, F. S. and Ladd, J. A., “Experimental & Numerical Investigation of Supersonic Impinging Jets,” AIAA Paper 2000-2224, AIAA, Fluids 2000 Conference, June, 2000, Denver, CO. (to appear in the AIAA Journal)
• Iyer, K. and Alvi, F. S.  “Flowfield Behavior of Supersonic Impinging Jets,” 51st Annual Meeting, American Physical Society, Division of Fluid Dynamics, Philadelphia, PA, Bulletin of the American Physical Society, Vol. 43, Nov. 1998.

• Krothapalli, A., Rajakuperan, E. Alvi, F. S. and Lourenco, L., “Flow field and Noise Characteristics of a Supersonic Impinging Jet,” AIAA 98-2239, June, 1998.
• Alvi, F. S., Krothapalli, A. and Strykowski, P. J., “Effect of Coflow on Counterflow Thrust Vectoring,” 50th Annual Meeting, American Physical Society, Division of Fluid Dynamics, San Francisco, CA, Bulletin of the American Physical Society, Vol. 42, Nov. 1997.
• Ramaswamy, M. A., Alvi, F. S. and Krothapalli, A., "Special 6-component Jet Rig Balance for Studying New Thrust Vectoring Concepts," 17th ICIASF Conference, Pacific Grove, CA, Sept.-Oct., 1997.
• Strykowski, P. J., Schmidt, G. F., Alvi, F. S. and Krothapalli, A., "Vectoring Thrust using Confined Countercurrent Shear Layers," 28th AIAA Fluid Dynamics Conference, AIAA 97-1997, July. 1997.
• Washington, D., Shih, C. and Alvi, F. S., "The use of Counterflow for Noise Suppression of a Supersonic Rectangular Jet," 35th AIAA Aerospace Sciences Meeting, AIAA 97-0149, Jan. 1997.
• Alvi, F. S., Strykowski, P. J., Washington, D. and Krothapalli, A., "Multi-Axis Fluidic Thrust Vectoring of Supersonic Jets via Counterflow," 35th AIAA Aerospace Sciences Meeting, AIAA 97-0393, Jan. 1997.
• Washington, D., Shih, C. and Alvi, F. S., and Krothapalli, "The Effect of Counterflow on the Acoustic Characteristics of a Mach 1.44 Rectangular Jet,"  49th Annual Meeting, American Physical Society, Division of Fluid Dynamics, Syracuse, NY, Nov. 1996.  Bulletin of the American Physical Society, Vol. 41, No. 9., Nov. 1996.
• Washington, D., Alvi, F. S., Krothapalli, A. and Strykowski, P. J., "3?D Thrust Vectoring of a Mach 2 Diamond Jet Using Counterflow," 48th Annual Meeting, American Physical Society, Division of Fluid Dynamics, Irvine, CA, Bulletin of the American Physical Society, Vol. 40, Nov. 1995.
• Alvi, F. S., Washington D. and Krothapalli, A., “The Flowfield Characteristics of a Mach 2 Diamond Jet,” 1st ASME/JSME Fluids Engineering and Laser Anemometry Conference, Forum on High Speed Jet Flows, FED Vol. 214, August 1995, pp. 127-132.
• Alvi, F. S., Krothapalli, A and Washington D., “Fluctuating Pressure Measurements in a Highly Compressible Countercurrent Turbulent Shear Layer,” 26th AIAA Fluid Dynamics Conference, AIAA Paper 95-2175, June 1995.
• Alvi, F. S. and Krothapalli, A, " Highly Compressible (Mc=2) Countercurrent Shear Layer," 47th Annual Meeting, American Physical Society, Division of Fluid Dynamics, Georgia Tech University, Bulletin of the American Physical Society, Vol. 39, Nov. 1994.
• Washington, D., Krothapalli, A., and Alvi, F. S., "Flow Visualization Study of a Mach 2.0 Diamond Shaped Jet", 47th Annual Meeting, American Physical Society, Division of Fluid Dynamics, Atlanta, GA, Bulletin of the American Physical Society, Vol. 39, Nov. 1994.
• Alvi, F. S. and Krothapalli, A, " Counterflowing Shear layer at a High Convective Mach Number (Mc=2)," 46th  Annual Meeting, American Physical Society, Division of Fluid Dynamics, University of New  Mexico, Bulletin of the American Physical Society, Vol. 38, Nov.  1993.
• Alvi, F. S., Settles, G. S and Weinstein, L. M., "A Sharp-Focusing Schlieren Optical Deflectometer,"  AIAA Paper 93-0629, Jan. 1993.
• Alvi, F. S. and Settles G. S., "Flowfield Structure of Shock Wave/Boundary-Layer Interactions Using Conical Shadowgraphy," 43rd Annual Meeting, American Physical Society, Division of Fluid Dynamics, Cornell University, Bulletin of the American Physical Society, Vol. 35, Nov. 1990.
• Alvi, F. S. and Settles, G. S., "Structure of Swept Shock Wave/Boundary-Layer Interactions Using Conical Shadowgraphy,"  21st AIAA Fluid Dynamics Conference, AIAA 90-1644, June, 1990.