1. A. N. Mikhalev, “Effect of the Reynolds number on the parameters of the near wake of supersonic cones,” Physical-Gasdynamic Ballistic Studies [in Russian], Nauka, Leningrad (1980), pp. 88–98.
2. G. I. Bagaev, V. A. Lebiga, V. G. Pridanov, and V. V. Chernykh, “Supersonic wind tunnel T-325 with reduced turbulence,” in: Aerodynamic Investigations [in Russian], Novosibirsk (1972), pp. 11–13.
3. A. Demetriades, “Experiments on the free shear layer between two supersonic streams,” AIAA Pap., No. 710 (1990).
4. Behrens, “Study of the far part of the wake behind cylinders, at hypersonic velocities. Part II. Stability,” AIAA J.,6, No. 2, 41–50 (1968).
5. A. Demetrides, “Hot-wire anemometer measurements in wakes behind thin bodies in a hypersonic flow,” Ibid.,2, No. 2, 28–35 (1964).