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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 1993 Volume 34, Issue 5, Pages 88–94 (Mi pmtf3983)

This article is cited in 1 paper

Numerical calculation of a three-dimensional laminar compressible boundary layer on profiled triangular wings with supersonic front edges

V. N. Vetlutskii, T. V. Poplavskaya

Novosibirsk

UDC: 532.526

Received: 03.02.1992
Accepted: 01.10.1992


 English version:
Journal of Applied Mechanics and Technical Physics, 1993, 34:5, 677–682


© Steklov Math. Inst. of RAS, 2025