1. Application of pulse facilities to inlet testing
2. A. S. Korolev, B. V. Boshenyatov, I. G. Drouker, and V. V. Zatoloka, Hot-shot Wind Tunnels as a Hardware for Aerodynamic Investigations (Nauka, Novosibirsk, 1978), 80 p. (in Russian)
3. B. V. Boshenyatov, B. N. Gilyazetdinov, and V. V. Zatoloka, “Experimental investigations of hypersonic inlets,”, in Aeromechanics (Nauka, Moscow, 1976), 98 p. (in Russian)
4. A. S. Antonov, B. V. Boshenyatov, B. N. Gilyazetdinov, B. N. Gutov, and V. V. Zatoloka, “Tests of hypersonic axisymmetric inlets of internal compression in the hypersonic hot-shot wind tunnel IT-301 at Mach number M = 11.5,” in Aerophysical Research (ITAM SB RAS, Novosibirsk, 1972), pp. 108–109. (in Russian)
5. D. M. Van Wie, F. T. Kwok, and R. F. Walsh, AIAA Paper 96-2914 (1996).