Geodesic
Solution of the problem of a wing oscillation in a supersonic gas flow
Dalʹnevostočnyj matematičeskij žurnal, Tome 7 (2007) no. 1, pp. 30-34 Cet article a éte moissonné depuis la source Math-Net.Ru

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The problem of a thin wing oscillation in a supersonic flow that was formulated in [1] is solved for all frequency intervals. 
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T. P. Arsent'ev; R. G. Barantsev. Solution of the problem of a wing oscillation in a supersonic gas flow. Dalʹnevostočnyj matematičeskij žurnal, Tome 7 (2007) no. 1, pp. 30-34. http://geodesic.mathdoc.fr/item/DVMG_2007_7_1_a2/

[1] R. G. Barantsev, “Vliyanie kriticheskikh chastot na postanovku zadachi o kolebanii tonkogo kryla v potoke gaza”, Dalnevostochnyi matematicheskii zhurnal, 5:1 (2004), 226–230

[2] Dzh. U. Mails, Potentsialnaya teoriya neustanovivshikhsya sverkhzvukovykh techenii, Fizmatgiz, M., 1963, 272 pp.

[3] R. G. Barantsev, “Metod poryadkovykh uravnenii”, Dalnevostochnyi matematicheskii zhurnal, 2:2 (2001), 5–9

[4] N. S. Koshlyakov, E. B. Gliner, M. M. Smirnov, Differentsialnye uravneniya matematicheskoi fiziki, GIFML, M., 1962

[5] I. S. Gradshtein, I. M. Ryzhik, Tablitsy integralov, summ, ryadov i proizvedenii, GIFML, M., 1962, 1100 pp.

[6] S. V. Vallander, Lektsii po gidroaeromekhanike, L., 1978, 296 pp.