1. G.I. Taganov, “Peculiar Properties of Flows in Supersonic Axial Compressors,” Tr. TsAGI (1951).
2. G.L. Grozdovskii, A.A. Nikol’skii, G.I. Svishchev, and G.I. Taganov, Supersonic Gas Flows within Perforated Boundaries [in Russian], Mashinostroenie, Moscow (1967).
3. G.Yu. Stepanov, Hydrodynamics of Turbomachinery Cascades [in Russian], Fizmatgiz, Moscow (1962).
4. O.K. Lawaczek, “Calculation of the Flow Properties Up- and Downstream of and within a Supersonic Turbine Cascade,” ASME Paper No. GT-47 (1972).
5. H.J. Lichtfuss and H. Starken, “Supersonic Cascade Flow,” in: Progr. Aerospace Sci. Vol. 15, Pergamon Press, Oxford (1974), p. 37.