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Novosibirsk. Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, No. 1, pp. 68–74, January–February, 1994.
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Vetlutskii, V.N., Poplavskaya, T.V. Computational analysis of a spatial compressed turbulent boundary layer on the upwind side of delta wings under supersonic flow. J Appl Mech Tech Phys 35, 69–74 (1994). https://doi.org/10.1007/BF02369753
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DOI: https://doi.org/10.1007/BF02369753