S. V. Kalinina, V. I. Kornilov, “Influence of the sweepback angle and the unit Reynolds number on boundary-layer transition at supersonic velocities”, Prikl. Mekh. Tekh. Fiz., 1973, Volume 14, Issue 1,Pages <nobr>159

JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 1973 Volume 14, Issue 1, Pages 159–162 (Mi pmtf7272)

Influence of the sweepback angle and the unit Reynolds number on boundary-layer transition at supersonic velocities

S. V. Kalinina, V. I. Kornilov

Novosibirsk

UDC: 533.6:532.526

Received: 29.05.1972

Fulltext: PDF file (818 kB)

English version: Journal of Applied Mechanics and Technical Physics, 1973, 14:1, 132–134