* Данный текст распознан в автоматическом режиме, поэтому может содержать ошибки

512 Литература 8-1. L i b r e s t u L. Asupra Matter u l n i neliniar al s t r u c t u r l o l cilintjrice, s u b t i r i , neorr.ogene. S t u d i i si Cercatorl de Mechanics A p l i c a t a , 13, u. 3, 1962 53. L e o n л i U R. H c d g e p c t h J. M . On panel f l u t t e r ant divergence of i n f i n i t e l y long unstiffened find ring-stiffened t h i n - w a l l e d c i r c u i t cylinders. N Л СА Rep- n. 1302, 1957, 86. [, i п (I Ii о 1 m U . S., К a n ft U. D., Л Ъ r a in s o n ll, N . Rrcatil­ i n g v i b r a t i o n of a circular c y l i n d r i c a l shell w i t h an internal l i q u i d . J. Aerospace ScL, v. 29, n. 9, 1962. 37. M i l e s J. w . Supersonic flutter of a c y l i n d r i c a l shell. J. Aeronaut, ScL, v. 24. n. 2, 1957; v . 25, n. 5, 195ft. 38. N e l s o n H, С , С u n n i n g h a m H . J. Theoretical investiga­ t i o n of f h K l c r of two-dimensional f l a t panels w i t h one surf «се exposed t o super sonic p o t e n t i a l i l o w . N АСА Rep. n, 1260, 1956. 89. К a 1 1 s к i S.. S o h r z E. Aero—megneto — f l u t t e r of a plate Пей past b y a perfectly conductive gas In magnetic field w i t h isolropic action. Pro­ ceedings of v i b r a t i o n problems, v. 3, n- 3. 1962. 91). V о s s H . M- The effect of an external supersonic flow on the v i b r a l i o r characteristics, of t h i n c y l i n d r i c a l shells. J. Aerospace ScL, v o l . 28, n. 12, 1961. 91. w e n - H w a - С h Breathing v i b r a t i o n s of a p a r t i a l l y f i l l e d c y l i n ­ d r i c a l t a n k - l i n e a r theory. Journal of A p p l . Mech., v, , n. 4, 1963.