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References 1 Kovasznay, L. S. G., Turbulence in supersonic flow, J. Aeronaut. Sci. 20, 657 (1953). 2 Ribner, H. S., Convection of a pattern of vorticity through a shock wave, NACA Rept. 1164 (1954). 3 Hollingsworth, M. A. and Richards, E. J., A schlieren study of the interaction between a vortex and a shock wave in a shock tube, Aeronautical Research Council Rept. 17985, Fluid Motion Sub-Committee 2323 (1955). 4 Hollingsworth, M. A. and Richards, E. J., On the sound generated by the interaction of a vortex and a shock wave, Aeronautical Research Council Rept. 18257, Fluid Motion SubCommittee 2371 (1956). 5 Ribner, H. S., The sound generated by interaction of a single vortex with a shock wave, University of Toronto, Institute of Aerophysics Rept. 61 (1959). 6 Ruetnik, J. R. and Witmer, E. A., Transient aerodynamics of two-dimensional airfoils, Part 2, Wright Air Development Center TR 54-368, AD151018 (1958). 7 Lamb, H., Hydrodynamics (Dover Publications, Inc., New York, 1945), 6th ed. Chap. VII, p. 232. 8 Abbott, I. H., von Doenhott, A. E., and Strivers, L. S., Jr., Summary of airfoil data, NACA Rept. 824 (1945). 9 Lighthill, M. J., Jet noise, AIAA J. 1, 1507-1517 (1963). 10 Powell, A., Theory of vortex sound, J. Acoust. Soc. Am. 36,177-195(1963). 11 Curie, N., The influence of solid boundaries upon aerodynamic sound, Proc. Roy. Soc. (London) A231, 505-514 (1955). 12 Lamb, H., Hydrodynamics (Dover Publications, Inc., New York, 1945) 6th ed. Chap XI, p. 592. 13 Roshko, A., On the development of turbulent wakes from vortex streets, NACA TN 2913, pp. 42-43 (1953). 14 Weeks, T. M. and Dosanjh, D. S., Interaction between an advancing shock wave and opposing jet flow, AIAA J. 1, 15271533 (1963). Birkhoff, G. and Zarantonello, E. H., Jets, wakes, and cavities, Applied Mathematics and Mechanics No. 2 (Academic Press Inc., New York, 1957), Chap. XIII, pp. 282-283.