1. A. Kantrowitz and C. Donaldson, Preliminary investigation of supersonic diffusers, NACA WRL-713, 1945.
2. D.M. Van Wie, F.T. Kwok, and R.F. Walsh, Starting characteristics of supersonic inlets, AIAA, ASME, SAE, and ASEE Joint Propuls. Conf. and Exhibit, 32nd, Lake Buena Vista, FL, July 1−3. AIAA Paper, 1996, No. 96−2914.
3. V.G. Gurylev, A.K. Ivanyushkin, and E.V. Piotrovich, Experimental investigation of the influence of the ReL number on the starting of inlets at high supersonic flow velocities, Uchenye zapiski TsAGI, Vol. 4, No. 1, P. 33–44.
4. A. Chevagin, Intake capability improvements in ramjet-type propulsion system, Paper of 28th Intern. Congress of the Aeronautical Sci., 2012.
5. F. Falempin, M.A. Goldfeld, Yu.V. Semenova, A.V. Starov, and K.Yu. Timofeev, Experimental study of different control methods for hypersonic air inlets, Thermophysics and Aeromechanics, 2008, Vol. 15, No. 1, P. 1–9.