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

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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/