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JOURNALS // Prikladnaya Mekhanika i Tekhnicheskaya Fizika // Archive

Prikl. Mekh. Tekh. Fiz., 1973 Volume 14, Issue 6, Pages 76–81 (Mi pmtf7393)

Numerical solution of the problem of the flow of a supersonic gas stream over the upper surface of a delta wing in the expansion region

G. P. Voskresenskii

Moscow

UDC: 533.6.011:51

Received: 24.05.1973


 English version:
Journal of Applied Mechanics and Technical Physics, 1973, 14:6, 798–802


© Steklov Math. Inst. of RAS, 2026