Dolling, D.S. and Murphy, M.T., "Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield," AIAA Journal, Vol. 21, No. 12, 1983, pp. 1628-1634. CrossRef
	Kistler, A.L., "Fluctuating Wall Pressure Under Separated Supersonic Flow", Journal of Acoustical Society of America, Vol. 36, March 1964, pp. 543-550. CrossRef
	Hadjadj, A., Dussauge, J.P. "Shock wave boundary layer interaction" Shock Waves, Vol. 19, pp. 449-452, 2009. CrossRef
	Dolling, D.S. and Murphy, M.T., "Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield," AIAA Journal, Vol. 21, No. 12, 1983, pp. 1628-1634. CrossRef
	Muck, K.C., Andreopoulos, J., and Dussuage, J.P., "Unsteady Nature of Shock-Wave/Boundary-Layer Interactions," AIAA Journal, Vol. 26, No. 2, 1988, pp. 179-187. CrossRef
	Dolling, D.S and Brusniak, L., "Separation Shock Motion in Fin, Cylinder, and Compression Ramp-Induced Turbulent Interactions," AIAA Journal, Vol. 27, No.6, 1989, pp. 734-742. CrossRef
	Blinde, P.L., Humble, R.A., Oudheusden, B.W. and Scarano, F., "Effects of Micro-Ramps on a Shock Wave/Turbulent Boundary Layer Interaction", Shock Waves, Vol. 19, pp. 507-520, 2009. CrossRef
	Babinsky, H., Makinson, N.J. and Morgan, N.J., "Micro-vortex Generator Flow Control for Supersonic Engine Inlets", AIAA Paper 2007-0521.
	Szwaba, R., "Shock Wave Induced Separation Control by Streamwise Vortices", Journal of Thermal Science, Vol. 14, No. 3, 2005, pp. 249-253. CrossRef
	Souverein, L.J. and Debiève, J. -F, "Effect of Air Jet Vortex Generators on a shock wave Boundary Layer Interaction, Experiments in Fluids, Vol. 49, 2010, pp. 1053-1064. CrossRef
	Delery, J.M., "A Physical Introduction to Control Techniques Applied to Turbulent Separated Flows", AIAA-2000-2606.
	Barter, J.W., Dolling, D.S., "Reduction of Fluctuating Pressure Loads in Shock/Boundary-Layer Interactions Using Vortex Generators", AIAA Journal, Vo. 33, No. 10, 1995, pp. 1842-1849. CrossRef
	Verma, S. B., Manisankar, C. and Raju, C., "Control of shock unsteadiness in shock boundary-layer interaction on a compression corner using mechanical vortex generators", Shock Waves, DOI 10.1007/s00193-012-0369-8.
	Raju, C. and Vishwanath, P.R., "Pressure-Sensitive Paint Measurements in a Blow-down Wind Tunnel", Journal of Aircraft, Vol. 42, No. 4, July-Aug. 2005.
	Van Driest, E.R., "Turbulent Boundary Layer in Compressible Flows," Journal of Aeronautical Sciences, Vol. 18, No. 3, 1951, pp. 145. CrossRef
	O'Donnell R.M., "Experimental Investigation at a Mach number of 2.41 of Average Skin-Friction Coefficients and Velocity Profiles for Laminar and Turbulent Boundary Layers and an Assesment of Probe Effects", NACA TN 3122, Jan 1954.
	Verma, S.B. and Gupta, V., "Supersonic Separation with Obstructions", AIAA Journal, 1996, Vol. 34, No. 4, pp. 849-850, DOI: 10.2514/3.13151. CrossRef
	Lin, C.C., Turbulent Flows and Heat Transfer, 1959.