Ostapenko, N. A.; Simonenko, A. M.; Chulkov, A. A. 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. Reviewer: V. I. Goncharenko (Kyïv) Cited in 3 Documents MSC: 76J20 Supersonic flows 76L05 Shock waves and blast waves in fluid mechanics Keywords:modes of streamlining of \(V\)-shaped wings; flow structure PDF BibTeX XML Cite \textit{N. A. Ostapenko} et al., Vestn. Mosk. Univ., Ser. I 2006, No. 4, 41--45 (2006; Zbl 1150.76430); translation in Mosc. Univ. Mech. Bull. 61, No. 4, 8--13 (2006) OpenURL