• Alvi, F. S. and Iyer, K., “Mean and Unsteady Properties of Supersonic Impinging Jets with Lift Plates,” AIAA Paper 99-1829, May, 1999.

• 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, Vol. 36, No. 2, March/April 1999, pp. 451-457.

• 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, pp. 279-281.

• 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.

• 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.

• 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.

• 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.

 

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