G. N. Dudin, “Flow in the hypersonic boundary layer on a finite triangular wing in the presence of an angle of attack”, Prikl. Mekh. Tekh. Fiz., 1983, Volume 24, Issue 3,Pages <nobr>108

JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 1983 Volume 24, Issue 3, Pages 108–113 (Mi pmtf5669)

This article is cited in 1 paper

Flow in the hypersonic boundary layer on a finite triangular wing in the presence of an angle of attack

G. N. Dudin

Moscow

UDC: 533.6.011.55

Received: 14.05.1982

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English version: Journal of Applied Mechanics and Technical Physics, 1983, 24:3, 383–388