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Some modes of supersonic streamlining of \(V\)-shaped wings with sliding. (Russian, English) Zbl 1150.76430

Vestn. Mosk. Univ., Ser. I 2006, No. 4, 41-45 (2006); translation in Mosc. Univ. Mech. Bull. 61, No. 4, 8-13 (2006).
The authors present results of numerical calculations of asymmetric streamlining of \(V\)-shaped wings adjacent to the front edges main shock wave. The calculations refer to the existence of specific streamlining modes discovered in the framework of linear theory and not described earlier in the literature.

MSC:

76J20 Supersonic flows
76L05 Shock waves and blast waves in fluid mechanics
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