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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 1985 Volume 26, Issue 5, Pages 23–29 (Mi pmtf5346)

This article is cited in 3 papers

Compressible laminar boundary layer on a delta wing with attached shock wave

V. N. Vetlutskii, T. V. Poplavskaya

Novosibirsk

UDC: 532.526

Received: 12.07.1984


 English version:
Journal of Applied Mechanics and Technical Physics, 1985, 26:5, 624–629


© Steklov Math. Inst. of RAS, 2025