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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 1994 Volume 35, Issue 1, Pages 68–74 (Mi pmtf3752)

Computational analysis of a spatial compressed turbulent boundary layer on the upwind side of delta wings under supersonic flow

V. N. Vetlutskii, T. V. Poplavskaya

Novosibirsk

UDC: 532.526

Received: 18.02.1993


 English version:
Journal of Applied Mechanics and Technical Physics, 1994, 35:1, 69–74


© Steklov Math. Inst. of RAS, 2025