![](/user_photo/_userpic.png)
книги / Нелинейные задачи динамики цилиндрических композитных оболочек
..pdf310.Dong S. В., Tso F. K. W.On a laminated orthotropic shell theory, including transverse shear deformation. —J. Appl. Mech. Trans. ASME. Ser, E, 1972, vol. 94, N4, p. 1091—1097.
311.Donnell L. H. Stability of thin-walled tubes under torsion. —NASAReports, 1933, N479.
312.Donnell L И. Anewtheory for the buckling of thin cylinders under axial compression and bending. —Trans. ASME, 1934, vol. 56, p. 795—806.
313.Dowell E. H., Ventres C. S. Modal equations for the nonlinear flexural vibra tions of a cylindrical shell. —Intern. J. Solids a. Structures, 1968, vol. 4, N10, p. 975-991.
314.DymC. L. Some new results for the vibrations of circular cylinders. —J. Sound a. Vibration, 1973, vol. 29, N2, p. 189—205.
315.El-Raheb M, Babcock C. D., jun. Some approximations in the linear dynamic equations of thin cylinders. —J. Sound a. Vibration, 1981, vol. 76, N4,
p.543—559.
316.Ertepinar A. Large amplitude radial oscillations of layered thick walled cy lindrical shells. — Intern. J. Solids a. Structures, 1977, vol. 13, N 8,
p.717—723.
317.Evan-Ivanowski R. M. On the parametric response of structures. —Appl. Mech. Rev., 1965, vol. 18, N9, p. 699—702.
318.Evensen D. A. Some observations on the nonlinear vibration of thin cylin drical shells. —AIAAJ„ 1963, vol. 1, N12, p. 2857—2858.
319.Evensen D. A. Nonlinear vibrations of an infinitely long cylindrical shell. — AIAAJ., 1968, vol. 6, N7, p. 1401—1403.
320.Evensen D. A., Fulton R. E. Some studies of the non-linear dynamic response of shell-type structures. —In: Dynamic stability structures. Proc. of an In tern. conf. / Ed. by G.Herrman. Oxford, 1967.
321.Fliigge W. Schwingungen zylindrischer Schalen. —Ztschr. Angew. Math. Mech., 1933, Bd 13, S. 425.
322.Flugge W.Stresses in shells. Berlin, Springer-Verl., 1973. —526 p.
323.Forsberg K. Influence of boundary conditions on the modal characteristics of thin cylindrical shells. —AIAAJ., 1964, vol. 2, N12, p. 2150—2157.
324.Forsberg R. Axisymmetric and beam-type vibrations of thin cylindrical shells. —AIAAJ., 1969, vol. 7, N2, p. 221—227.
325.Fujii T., Miki M. The studies on impact behavior for unidirectional fiber reinforced plastics. —Mem. Fac. Eng., Osaka City Univ., 1973, N 14, p. 25—35.
326.Gazis D. C. Three-dimensional investigation of the propagation of waves in hollow circular cylinders. 1. Analytical foundation. 2. Numerical results. — J. Acoustical Soc. Amer., 1959, vol. 31, N5, p. 568—573; 573—578.
327.Ginsberg /. H. Non-linear resonant vibrations of infinitely long cylindrical shells. —AIAA J., 1972, vol. 10, p. 979—980.
328.Ginsberg J. H. Large amplitude forced vibrations of simply supported thin cylindrical shells. —Trans. ASME. Ser. E, 1973, vol. 40, N2, p. 471—477.
329.Gottenberg W.G. Experimental study of the vibrations of a circular cylindri cal shell. —J. Acoustical Soc. Amer., 1960, vol. 32, N8, p. 1002—1006.
330.Greenberg J. B., Stavsky Y.Buckling and vibration of orthotropic composite cylindrical shells. —Acta Mech., 1980, vol. 36, N 1/2—3/4, p. 15—29.
331.Greenberg J. B., Stavsky Y. Vibrations of axially compressed laminated orthotropic cylindrical shells, including transverse shear deformation. —Acta Mech., 1980, vol. 37, N1—2, p. 13—28.
332.Greenberg J. B., Stavsky Y. Vibrations of laminated filament-wound cylin drical shells. —AIAAJ., 1981, vol. 19, N8. p. 1055—1062.
333.Greenberg J. B., Stavsky Y.Stability and vibrations of compressed, aelotropic, composite cylindrical shells. —Trans. ASME. J. Appl. Mech., 1982, vol. 49, N4, p. 843-848.
334.Greenspon J. Flexural vibrations of thick walled circular cylinders. —In: Proc. 3rd U. S. nat. congr. appl. mech. New York, 1958, p. 163—173.
335.Greenspon J. Vibrations of thick cylindrical shells. —J. Acoustical Soc. Amer., 1959, vol. 31, N12, p. 1682—1683.
336.Greenspon J. Flexural vibrations of a thick walled circular cylinder according to the exact theory of elasticity. —J. of Aero-Space Sci., 1960, vol. 27, N1, p. 37—40.
337.Greenspon J. Vibrations of a thick-walled cylindrical shell —comparison of the exact theory with approximate theories. —J. Acoustical Soc. Amer., 1960, vol. 32, N5, p. 571—578.
338.Greif R. Inertia effects in the dynamic response of a cylindrical shell. — AIAAJ., 1966, vol. 4, N6, p. 1105—1106.
339.Gryboi Ryszard. Statecznosc konstrukcji pod obciazeniem uderzoniowym. Warszawa; Poznan, Pol. Akad. Nauk, 1980. 424 s.
340.Guess T. R. Biaxial testing of composite cylinders: experimental —theoreti cal comparison. —Composites, 1980, vol. 11, N3, p. 139—148.
341.Hahn H. T., Tsai S. W.On the behavior of composite laminates after initial failures. —J. Composite Materials, 1974, vol. 8, N3, p. 288—305.
342.Harari A., Sandman В. E. Experimental and theoretical dynamic analysis of carbon-graphite composite shells. —Shock a. Vibration Bull., 1978, vol. 48, N3, p. 33-37.
343.Harding J., Welsh L. M.Atensile testing technique for fiber-reinforced com posites at impact rates of strain. —J. Materials Sci., 1983, vol. 18, N6, p. 1810—1826.
344.Herrmann G., Mirsky I. Three-dimensional and shell-theory analysis of axially symmetric motions of cylinders. —Trans. ASME. Ser.E. J. Appl. Mech., 1956, vol. 23, N4, p. 563—568.
345.Hoff N. J. The accuracy of Donnel’s equations. —Trans. ASME. Ser.E. J. Appl. Mech., 1955, vol. 22, N3, p. 329—334.
346.Hoff N. Dynamic stability of structures. —In: Dynamic stability of struc tures. Oxford etc., Pergamon Press, 1967, p. 7—41.
347.Hsu T.-М., Wang J. Rotationally symmetric vibrations of orthotropic layered cylindrical shells. —J. Sound a. Vibration, 1971, vol. 16, N4, p. 473—487.
348.Hughes T.J. R., Liu W.K-, Levit 1. Nonlinear dynamic finite element analysis of shells. —In: Nonlinear finite element analysis. Structural mechanics. Proc. Europ. —U. S. Workshop, Bochum, 1980. Berlin etc., 1981, p. 151—168.
349.Humpreys J. S., Sve C. Dynamic buckling of cylinders under axial shock-tube loading. —AIAAJ., 1966, vol. 4, N8, p. 1477—1480.
350.Hutchinson J. W., Budiansky B. Dynamic buckling estimates. —AIAAJ., 1966, vol. 4, N3, p. 525-530.
351.Iyer S. H., Simmonds S. H. The accuracy of Donnel’s theory for very high harmonic loading of closed cylinders. —Trans. ASME. Ser.E, 1972, vol. 39, N3, p. 200—202.
352.Jones J. P., Whittier J. S. Axially symmetric motions of a two-layered Ti moshenko-type cylindrical shell. —Trans. ASME. Ser.E. J. Appl. Mech., 1966, vol. 33, N4, p. 838-844.
353.Jones J. P., Whittier J. S. Dynamics of a flexibly bonded two-layered Ti- moshenko-type cylindrical shell. —AIAAJ., 1969, vol. 7, N2, p. 244—250.
354.Jones R. M., Morgan H. S. Buckling and vibration of cross-ply laminated circular cylindrical shells. —AIAAJ., 1975, vol. 13, N5, p. 664—671.
355.Kagawa Y. Non-axially symmetrical vibrations of sandwich cylindrical shells. —J. Sound a. Vibration, 1967, vol. 7, N1, p. 41—50.
356.Kawata K-, Hashimoto S., Takeda N. Mechanical behaviours in high velocity tension of composites. —In: Progr. sci. and eng. compos. Proc. 4th Intern. Conf., ICCM-IV. Tokyo, 1982, vol. 1, p. 829—836.
357.Kawata K., Hondo A., Hashimoto S. et al. Dynamic behaviour analysis of composite materials. —In: Composite materials. Mechanics, mechanical pro perties and fabrics. Jap.-US Conf., Tokyo, 1981. Barking, 1981, p. 2—11.
358.KimH. C., Park Y.H. Impact behaviour of quasi-isotropic CFRP laminate. — In: Progr. sci. and eng. compos. Proc. 4th Intern, conf., ICCM-IV. Tokvo, 1982, vol. 1, p. 895—899.
359.Klein S. Vibration of multilayer shells of revolution under dynamic and impulsive loading. —Shock a. Vibration Bull., Washington," 1966, vol. 35, N3, p. 27—44.
360.Koiter W.T. On the nonlinear theory of thin elastic shells, 1, 2, 3. —Proc.
K.Nederl. Akad. Wet., 1966, vol. B69, N1, p. 1—17; 18—32; 33—54.
361.Kousiounelos P. N.. Williams J. H„ jun. Dynamic fracture of unidirectional graphite fiber composite strips. —Intern. J. Fractures, 1982, vol. 20, N 1,
p.47-63.
362.Libai A. Nonlinear shell dynamics—intrinsic and semi-intrinsic approaches. — Trans. ASME. Ser.E, 1983, vol. 50, N3, p. 531—536.
363.Libai A., Simmonds I. G.Nonlinear elastic shell theory. —Adv. Appl. Mech., 1983, vol. 23, p. 271—371.
364.Lifshitz J. M. Impact strength of angle ply fiber reinforced materials. —J. Composite Materials, 1976, vol. 10, N1, p. 92—101.
365.Lifshitz J. M„ Gilat A. Experimental determination of the nonlinear sheai behavior of fiber-reinforced laminae under impact loading. —Experimental Mech., 1979, vol. 19, N12, p. 444—449.
366.Lin T„ Morgan C. Astudy of axisymmetric vibrations of a cylindrical shell as affected by rotatory inertia and transverse shear. —Trans. ASME. Ser.E.
J.Appl. Mech., 1956, vol. 78, N2, p. 255-261.
367.Lindberg H. E. Buckling of a very thin cylindrical shell due to an impulsive pressure. —Trans. ASME. Ser.E. J. Appl. Mech., 1964, vol. 31, N 2,
p.267—272.
368.Lindberg И. E., Herbert R. E. Dynamic buckling of a thin cylindrical shell under axial impact. —Trans. ASME. Ser.E. J. Appl. Mech., 1966, vol. 33, N1, p. 105—113.
369.Loo T. T. An extension of Donnell’s equations for circular cylindrical shell. —
J.Aeronautical Sci., 1957, vol. 24, N5, p. 390—391.
370.Love A. On the small free vibrations and deformation of thin elastic shell. — Phil. Trans. Rcy. Soc., 1888, vol. 179 (A).
371.Marguerre K. Zur Théorie der gekrümmten Platte grober Formanderung. — In: Proc. 5th Intern, congr. appl. mech., Cambridge (Mass.), 1938. New York, J. Wiley a. Son, 1939, p. 93—101.
372.Matsuzaki T., Kobayashi S. Atheoretical and experimental study of the non linear flexural vibration of thin circular cylindrical shells with clamped ends. —J. Jap. Soc. Aeronautical a. Space Sci., 1970, vol. 12, N 21,
p.55—62.
373.Maymon G., Libai A. Dynamics and failure of cylindrical shells subjected to axial impact. —AIAAJ., 1977, vol. 15, N11, p. 1624—1630.
374.Afc Ivor /. K. The elastic cylindrical shell under radial impulse. —Trans. ASME. Ser.E. J. Appl. Mech., 1966, vol. 33, N4, p. 831—837.
375.Me Ivor /. K., Lovell E. G. Dynamic response of finite-lenght cylindrical shells to nearly uniform radial impulse. —AIAA J., 1968, vol. 6, N 12,
p.2346—2351.
376.Mente L. J. Dynamic nonlinear response of cylindrical shells to asymmetric pressure loading. —AIAAJ., 1973, vol. 11, N6, p. 793—800.
377.Mettler E. Stability and vibration problems of mechanical systems under har monic excitation. —In: Dynamic stability of structures. Oxford; New York, Pergamon Press, 1966.
378.Meyer A., Dôhler.B., Skurt L. Simultané Algoriihmen fiir groBdimensionierte Eigenwertproblem und ihre Anwendung auf das Schwingungsproblem. — Wiss. Schriftenr. Techn. Hochsch. Karl-Marx-Stadt, 1983, N8, S. 90.
379.Mindlin R. D. Influence of rotatory inertia and shear on flexural motions of isotropic, elastic plates. —Trans. ASME. Ser.E. J. Appl. Mech., 1951, vol. 73, N1, p. 31-38.
380.Mindlin R. D„ Bleich H. H. Response of an elastic cylindricalshell to a transverse step shock wave. —Trans. ASME. Ser.E. J. Appl. Mech., 1953, vol. 20, N2, p. 189—195.
381. Mirsky |
1. Vibrations'of orthotropic, thick, cylindrical shells. —J. Acoustical |
||||||||||||
• • |
Soc. Amer., 1964, vol. 36, N1, p. 41—51. |
|
|
|
|
|
|
||||||
382. Mirsky I., Herrmann G.Nonaxially symmetric motions of cylindrical shells. — |
|||||||||||||
|
J. Acoustical Soc. Amer., 1957, vol. 29, N10, p. 1116—1123. |
|
cylindrical |
||||||||||
383. Mirsky |
|
Herrmann D. Axially symmetric motions |
|
of thick |
|||||||||
|
shells. —Trans. ASME. Ser.E. J. Appl. Mech., 1958, vol. 80, N1, p. 97—103. |
||||||||||||
384. Morley |
L. S. B. An |
improvement on Donnel’s approximation |
for |
thin-walled |
|||||||||
|
circular cylinders. ^ |
Quart. J. Mech. Appl. Math., |
1959, |
vol. |
12, pt 1, |
||||||||
|
p. 89-99. |
|
|
|
|
|
|
on the transient res |
|||||
385. Mortimer R. W., BlumA. The effect of pulse duration |
|||||||||||||
|
ponse |
of |
cylindrical |
shells |
subjected to axial impact. —Trans. |
ASME. |
|||||||
|
Ser. E, 1974, vol. 41, N1, p. 312—313. |
|
|
|
|
cylindrical |
|||||||
386. Mortimer R. W„ Rose |
J. L, Chou P. C. Longitudinal impact of |
||||||||||||
|
shells. —Experimental Mech., 1972, vol. 12, N1, p. 25—31. |
|
|
|
|||||||||
387. Naghdi P. M.Some aspects |
of the nonlinear theory of elastic shells. —Bull. |
||||||||||||
|
Acad. Pol. Sci. Ser. Sci. Techn., 1964, vol. 12, N11a, suppl., p. 26—27. |
||||||||||||
388. Naghdi P. M., |
Cooper R. M. Propagation |
of elastic |
waves |
in |
cylindrical |
||||||||
|
shells, including the effects of transverse shear and rotatory inertia. —J. |
||||||||||||
|
Acoustical Soc. Amer., 1956, vol. 28, N1, p. 55—63. |
|
|
|
|
shells |
|||||||
389. Naghdi P. M., |
Nordgren R. P. On the nonlinear theory of elastic |
||||||||||||
|
under the |
Kirchhoff hypothesis. —Quart. Appl. Math., |
1963, vol. 21, N 1, |
||||||||||
|
p. 49—59. |
|
|
S. B., Kalra R. D. Vibrations and |
|
waves in |
laminated |
||||||
390. Nelson |
R. B., Dong |
|
|||||||||||
|
orthotropic circular cylinders. —J. Sound |
a. Vibration, |
1971, vol. 18, N3, |
||||||||||
|
p. 429-444. |
|
|
|
|
large rotation shell theories in |
|||||||
391. Nolte |
L.-P., Stumpf H. Energy-consistent |
||||||||||||
|
Langrangean description. —Mech. Research Communications, |
1983, vol. 10, |
|||||||||||
|
N4, p. 213—221. |
|
|
transverse vibrations of orthotropic |
cylindrical |
||||||||
392. NowinskiJ. |
L. Nonlinear |
||||||||||||
|
shells. —AIAAJ., 1963, vol. 1, N3, p. 617—620. |
|
shells for buckling |
||||||||||
393. Nshaniati Y.S., Pappas M.Optimal laminated composite |
|||||||||||||
|
and vibration. —AIAA |
1983, vol. 21, N3, p. 430—437. |
|
|
|
|
|||||||
394. Oliira H., Uda N. On the knee-point of cross-ply composite. —In: Progr. |
|||||||||||||
|
sci. and eng. composites. Proc. 4th Intern, conf. ICSS-IV. Tokvo, 1982, vol. 1, |
||||||||||||
|
p. 473—480. |
|
|
|
Mori T. Impact fatigue |
strength and |
reliabi |
||||||
395. Okabe N.. Yano T., Kamata |
|||||||||||||
|
lity for fiber reinforced |
epoxy resin laminates subjected |
to repeated |
impact |
|||||||||
|
loads. |
— |
J.Soc. Materials |
Sci., Jap., 1982, vol.31, N351, p. 1210—1216. |
|||||||||
396. Olson |
M. |
|
D.Some |
experimental observations onthe nonlinear vibration of |
|||||||||
|
cylindrical shells. —AIAAJ., 1965, vol. 3, N9, p. 1175—1177. |
|
|
|
|||||||||
397. Pietraszkiewicz |
W.On |
consistent approximations in the |
geometrically non |
||||||||||
|
linear theory of shells. —Mitt. Inst. Mech. Ruhr-Univ. Bochum, 1981, N26, |
||||||||||||
|
S. 39. |
|
|
W.Asimplest consistent version of the |
geometrically non |
||||||||
398. Pietraszkievicz |
|||||||||||||
|
linear theory of elastic shells undergoing large/small rotations. —Ztschr. |
||||||||||||
|
Angew. Math. Mech., 1983, Bd 63, N4, S. 200—202. |
|
curvature in large |
||||||||||
399. Prathap |
G., Pandalai K. A. The role of median surface |
||||||||||||
|
amplitude flexural vibrations of thin shells. —J. Sound a. Vibration, 1978, |
||||||||||||
|
vol. 60, N1, p. 119—131. |
|
|
|
|
|
|
|
400.Puppo A. H., Evensen H. A. Strength of anisotropic materials under combi ned stresses. —AIAAJ., 1972, vol. 10, N4, p. 468—474.
401.Radwan H. R.t Genin /. Nonlinear vibrations of thin cylinders. —Trans. ASME. Ser. E, 1976, vol. 43, N2, p. 370—372.
402. |
Radwan H. R„ Genin /. Dynamic instability in cylindrical shells. —J. Sound |
|
403. |
a. Vibration, 1978, vol. 56, N3, p. 373—382. |
|
Raj R. G., Manocha |
L M., Bahl O. P„ Verma D. S. Impact strength and |
|
1 |
fracture of glass fibre |
rèinforced epoxy composites. —Fibre Sci. a. Techtiol., |
|
1982, vol. 17, N2, p. 141-^148. |
404.Rand R. A., Shen С. N. Optimumdesign of composite shells subject to na> tural frequency constraints. —Computers a. Structures, 1973, vol. 3, N2, p. 247—263.
405.Rao S. Y. V.К■Vibrations of layered shells with transverse shear and ro tatory inertia effects. —J. Sound a. Vibration, 1983, vol. 86, N1, p. 147—150.
406.Rath В. K., Das Y.C. Vibration of layered shells. —J. Sound a. Vibration, 1973, vol. 28, p. 737-757.
407.Rayleigh J. W.S. The theory of the sound. 1929, vol. 1. London, Macmillan [Русский перевод: Релей Д. В. Теория звука. T. 1. —М.: Гостехиздат, 1940. —499 с.]
408.Rhodes М.D., Williams J. G., Starnes J. H., jun. Low-velocity impact damage in graphite-fiber reinforced epoxy laminates. —In: Techn. Proc. 34th Annu. conf. reinforced plastics/composites Inst. Reinf. Future, NewOrleans, 1979. NewYork, s. a., p. 20D/1—20D/10.
409.RotemA., Hashin Z. Failure modes of angle-ply laminates. —J. Composite Materials, 1975, vol. 9, p. 191—206.
410.Roth R. S., Klosner J. M. Nonlinear response of cylindrical shells subjected to dynamic axial loads. —AIAAJ., 1964, vol. 2, N 10, p. 1788—1794.
411.Rowlands R. E. Analytical —experimental correlation of polyaxial states of stress in thornel-epoxy laminates. —Experimental Mech., 1978, vol. 18, N7, p. 253—260.
412.Roylance D. Stress wave damage in graphite/epoxy laminates. —J. Com posite Materials, 1980, vol. 14, p. Ill—119.
413.Sanders J. L. Non-linear theories for thin shells. —Quart. Appl. Math., 1963, vol. 21, N1, p. 21—36.
414.Sayers К. H.t Harris B. Interlaminar shear strength of a carbon fibre rein forced composite material under impact conditions. —J. Composite Materials, 1973, vol. 7, N2, p. 129—136.
415.Schmitt A. F. Dynamic buckling tests of aluminum shells. —Aeronautical Eng. Rev., 1956, vol. 15, N9, p. 54—56.
416.Shafer В. P. Two-dimensional stress wave propagation in thick multilayered cylindrical shells. —In: AIAAstructure dynamics and aeroelasticity specialist conf., AIAA. New York, 1969, p 162—173.
417.Sharma С. B. An analytical vibration study of thin circular cylinders. —In: Recent advances in structural dynamics. Papers intern, conf. Southampton, 1980, vol. 1, p. 61—72.
418.Shirakawa K. Dynamic stability of cylindrical shells taking into account in-plane inertia and in-plane disturbance. —Bull. JSME, 1980, vol. 23, N176, p. 163—169.
419.Shirakawa K. Effects of shear deformation and rotatory inertia on vibration and buckling of cylindrical shells. —J. Sound a. Vibration, 1983, vol. 91, N3, p. 425—437.
420.Shivakumar K. N., Krishna M. A. V. Vibrations of multifiber composite shells —some numerical results. —J. Structural Mech., 1976, vol. 4, N4,
p.379—393.
421.Smith P. W.Phase velocities and displacement characteristics of free waves in a thin cylindrical shell. —J. Acoustical Soc. Amer., 1955, vol. 27, N6,
p.1065—1072.
422.Smith P. W.Vibrations of cylindrical shells. —J. Acoustical Soc. Amer., 1958, vol. 30, N1, p. 83—84.
423.Soedel W.On the vibration of shells with Timoshenko-Mindlin type shear deflections and rotatory inertia. —J. Sound a. Vibration, 1982, vol. 83, N1, p. 67—79.
424.Soldatos К. P. On the buckling and vibration of antisymmetric angle-ply laminated circular cylindrical shells. —Intern. J. Eng. Sci., 1983, vol. 21, N3, p. 217—222.
425.Stavsky Y., Loewy R. On vibrations of heterogeneous orthotropic cylindrical shells. —J. Sound a. Vibration, 1971, vol. 15, N2, p. 235—256.
426.Stellbrink К. On the behaviour of impact damaged CFRP laminates. —Fibre Sci. a. Technol., 1983, vol. 18, N2, p. 81—94.
427.Stevens К. К■On the parametric excitation of a viscoelastic column. —AIAA J„ 1966, vol. 4, N12, p. 2111—2116.
428.Stevens К■К. Transverse vibration of a viscoelastic column with initial curvatere under periodic axial load. —Trans. ASME. Ser.E. J. Appl. Mech., 1969, vol. 36, N4, p. 814—818.
429.Stevens /(. K. On the experimental determination of instability regions in rheolinear vibration problems. —Trans. ASME. Ser. E, 1972, vol. 39, N3, p. 831—832.
430.Stevens K. /(., Evan-Iwanowski R. M. Parametric resonanse of viscoelastic columns. —Intern. J. Solids a. Structures, 1969, vol. 5, N7, p. 755—765.
431.Sun С. T., Sun P. W.Laminated composite shells under axially symmetric dynamic loadings. —J. Sound a. Vibration, 1974, vol. 35, N3, p. 395—415.
432.Sun С. T., Sun P. W.Forced vibration of laminated composite cylindrical shells. —J. Math. Phys. Sci., 1975, vol. 9, N1, p. Ill—133.
433.Sun С. T„ Whitney J. M. Axisymmetric vibrations of laminated composite cylindrical shells. —J. Acoustical Soc. Amer., 1974, vol. 55, p. 1238—1246.
434.Tamura Y.S., Babcock C. D. Dynamic stability of cylindrical shells under step loading. —Trans. ASME. Ser. E, 1975, vol. 42, N1, p. 190—194.
435.Tennyson R. C. Buckling of laminated composite cylinders: a review. — Composites, 1975, vol. 6, N1, p. 17—24.
436.Tennyson R. C. Interaction of cylindrical shell buckling experiments with theory. —In: Theory of shells. North-Holland Publ. Co., 1980, p. 65—116.
437.Tennyson R. C., Tulk J. D. Dynamic stability of circular cylindrical shells. — In: Proc. 3rd Canad. congr. applied mechanics. Calgary, 1973, p. 355—356.
438.Tennyson R. C., Tulk J. D., Ricciatti R. Analysis of the collapse of cylindri cal shells using high-speed photography. —J. Soc. Motion Pictures a. Te levision Eng., 1971, vol. 80, N6, p. 477—481.
439.Timoshenko S. P. On the correction for shear of the differential equations for transverse vibrations of prismatic bars. —Philos. Mag., 1921, ser. 6, vol. 41, p. 744—746.
440.Timoshenko S. P. On the transverse vibrations of bars of uniform cross sec tion. —Philos. Mag., 1922, ser. 6, vol. 43, p. 125—131.
441.Timoshenko S. Theory of plates and shells. NewYork. Me Graw-Hill, 1940. 440 p.
442.Tobias S. A. Atheory of imperfection for the vibrations of elastic bodies of revolution. —Engineering, 1951, vol. 172, N4470, p. 409—410.
443.Tsai S. W., Wu E. M. Ageneral theory of strength for anisotropic mate rials. —J. Composite Materials, 1971, vol. 5, p. 58—80.
444.Tsao C. H. Strain-displacement relations in large displacement theory of shells. —AIAA J., 1964, vol. 2, N11, p. 2060—2062.
445.Tsuboi Y., Tosaka N. Nonlinear theory of thin elastic shells. —Technol. Rep. Tohoku Univ., 1970, vol. 35, N2, p. 87—111.
446.Utida J., Sezawa K. Dynamical stability of a column under periodic longi tudinal forces. —Rep. Aeronautical Research Inst. (Tokyo), 1940, vol. 15,
p.139—183.
447.Valid R. An intristic formulation for the nonlinear theory of shells and some approximations. —Computers a. Structures, 1979, vol. 10, N1/2, p. 183—194.
448.Vanderpool M. £., Bert C. W.Vibration of a materially monoclinic, thickwall circular cylindrical shell. —AIAAJ., 1981, vol. 19, N5, p. 634—641.
449.Vijayaraghavan A., Evan-Iwanowski R. M. Parametric instability of circular cylindrical shells. —Trans. ASME, Ser. E, 1967, vol. 34, N4, p. 985—990.
450.Warburton G. B. Vibration of thin cylindrical shells. —J. Mech. Eng. Sci., 1965, vol. 7, N4, p. 399—407.
451.Warburton G. В., Soni S. R. Resonant response of orthotropic cylindrical shells. —J. Sound a. Vibration, 1977, vol. 53, N I, p. 1—23.
452.Weidenhammer F. Nichtlineare Biegenschwingungen des axialpulsierend belasteten Stabes. —Ing. Arch., 1952, Bd 20, S. 315—330.
453.Weingarten V.I. Free vibrations of multilayered cylindrical shells. —Expe rimental Mech., 1964, vol. 4, N7, p. 200—205.
454.Weingarten V. /. Free vibration of thin cylindrical shells. —AIAAJ., 1964, vol. 2, N4, p. 717—722.
455.White J. C. The flexural vibrations of thin laminated cylinders. —Trans. ASME. Ser. B, 1961, vol. 83, N4, p. 397-402.
456.Whittier J. S., Jones J. P. Axially symmetric wave propagation in a two layered cylinder. —Intern. J. Solids a. Structures, 1967, vol. 3, N 4, p. 657—675.
457.Wilcox M. W., Abhat О. B. Dynamic response of laminated composite shells under radial or hydrostatic pressure. —Trans. ASME. Ser. J. J. Pressure Vessel Technol., 1974, vol. 96, p. 299—304.
458.Wood J. D., Koval L. R. Buckling of cylindrical shells under dynamic loads. —AIAAJ., 1963, vol. 1, N11, p. 2576—2582.
459.Wu E. M. Optimal experimental measurements of anisotropic failure ten sors. —J. Composite Materials, 1972, vol. 6, p. 472—489.
460.Yao J. C. Dynamic stability of cylindrical shells under staticand periodic axial and radial loads. —AIAAJ., 1963, vol. 1, N6, p. 1391—1396.
461.Yao J. C. Non-linear elastic buckling and parametric excitation of a cylinder under axial loads. —Tràns. ASME. Ser. E. J. Appl. Mech., 1965, vol. 32, N1, p. 109—115.
462.Yi-Yuan Yu. Free vibrations of thin cylindrical shells having finite length with freely supported and clamped edges. —Trans. ASME. Ser. E. J. Appl. Mech., 1955, vol. 22, N4, p. 547—552.
463.Yi-Yuan Yu. Vibrations of thin cylindrical shells analysed by means of Don nell-type equations. —J. Aero-Space Sci., 1958, vol. 25, N 11, p. 699—715.
464.Yi-Yuan Yu. Vibrations of elastic sandwich cylindrical shells. — Trans. ASME. Ser. E. J. Appl. Mech., 1960, vol. 82, N4, p. 653—662.
465.Zerna W.Über eine nichtlineare allgemeine Theorie der Schalen. —In: Proc. IUTAM Symp. theory thin elastic shells, Delft, 1959. Amsterdam, 1960, p. 34-42.
466.Zimcik D. G., Tennyson R. C. Stability of circular cylindrical shells under transient axial impulsive loading. —AIAA J., 1980, vol. 18, N6, p. 691—699.
предметный указатель
Аппроксимация |
|
|
|
|
|
|
|
|
|
|
|
|||
конечно-разностная 162, 179 |
|
|||||||||||||
перемещений 20, 22, 26 |
|
|
109, 122, |
|||||||||||
прогиба |
10, |
13, |
|
107, |
108, |
|||||||||
123, |
125, |
128, |
|
130, |
|
133, |
152, |
153, |
||||||
175 |
|
|
|
|
|
107, |
|
125, |
129, |
133, |
||||
двучленная |
|
|
||||||||||||
135, 153, 183-185 |
|
|
|
|
|
|||||||||
Кармана—Цзяня |
|
109 |
133, |
152, |
||||||||||
многочленная |
129, |
|
||||||||||||
156, 185, 188, 191,194,204—209 |
||||||||||||||
одночленная |
|
131, 188, 189, 191, |
||||||||||||
194, |
199, 204—209, 215, 222 |
|||||||||||||
трехчленная |
|
|
107 |
|
|
|
|
|
|
|
||||
четырехчленная 123 |
|
|
|
|
||||||||||
Банк данных |
158 |
|
|
|
|
|
|
|
|
|
|
|||
Биения |
109, 128, 129, 134 |
|
|
|
|
|||||||||
Вектор |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
напряжения 33 |
|
|
|
|
|
|
|
|
|
|
||||
ограничений |
145 |
|
|
|
|
|
|
|
|
|||||
перемещения |
19, 20, 50 |
|
146—149 |
|||||||||||
проектных |
параметров |
|
||||||||||||
Взаимодействие |
гармоник |
129 |
|
|||||||||||
окружных 185 |
|
|
|
|
|
|
|
|||||||
осевых |
185 |
|
и |
|
|
иеосесиммет- |
||||||||
осесимметричной |
|
|
||||||||||||
ричной форм |
182, 200 |
|
|
|
|
|
||||||||
форм колебаний |
108 |
|
|
|
|
|
|
|||||||
Взаимосвязанность |
|
гармоник |
|
|||||||||||
окружных |
122, 155, |
|
184, 188, 191, |
|||||||||||
195, 199—206, 209, 214 |
|
|
|
|
||||||||||
осевых |
122, 188, 199, 200 |
|
|
|||||||||||
Внешнее давление 9, 14, 46, 83—85, |
||||||||||||||
152, 156 |
|
|
|
152, |
153, |
|
156, |
189, |
||||||
динамическое |
|
|||||||||||||
192, |
193, |
203, |
207, |
209, |
210, |
212, |
||||||||
217, |
224, |
229, |
238, |
|
240, |
243, |
247, |
|||||||
248, 251—254, 256—258, 260, 262, |
||||||||||||||
263 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
критическое |
|
|
|
156, 206 |
|
|
||||||||
динамическое |
|
|
||||||||||||
статическое 203, 239, 240 |
|
|||||||||||||
Внутреннее давление 9, 214, 226 |
|
|||||||||||||
Волны |
|
|
|
|
8, 65, 66 |
|
|
|
|
|||||
гармонические |
|
|
|
|
||||||||||
ударные 9 |
|
|
|
|
|
|
|
|
|
|
|
|||
Волокна |
армирующие 140, 146 |
|
||||||||||||
Время релаксации |
|
120 |
|
|
|
|
|
|
|
|||||
Выпучивание |
|
|
13, |
152—154, |
156, |
|||||||||
динамическое |
|
|||||||||||||
158, |
165, |
183—185, |
|
195, |
196, 202, |
|||||||||
217, 218, 253 |
|
|
|
|
|
|
|
|
|
|
||||
191544 |
|
|
|
|
|
|
|
|
|
|
|
неосесимметричное |
10, |
13, |
152, |
|||
154, |
156, |
184, |
185, |
195, |
200, |
233, |
235, 238, 239, 241 |
|
|
|
|||
осесимметричное 13, 165, 183, 233 |
Деформации |
|
|
|
|
|
|
|
|
|
||
дополнительные 47 |
|
|
|
|
|
||||||
изгнбные 67, 104, 166, 180, 231, |
|||||||||||
243 |
|
17 |
|
|
|
|
|
|
|
|
|
конечные |
|
|
|
|
|
|
|
|
|||
мембранные 39, 53, 67 |
|
|
|
|
|||||||
начальные 45 |
|
|
159, |
178, |
181, |
||||||
неосеснмметричные |
|||||||||||
241, 243, 263 |
|
|
10, |
178, |
180 |
|
|||||
осесимметричные |
203, |
||||||||||
пластические |
|
156, |
170, |
201, |
|||||||
206, 207 |
|
|
|
|
|
11—13, 15, 24, |
|||||
поперечных сдвигов |
|||||||||||
28, 41, 51, 55, 64-66, 88, 89, 94, |
|||||||||||
96, |
105, |
106, 218, 220, 221 |
|
|
|||||||
сдвиговые |
113, 114, 117, 259 |
|
|||||||||
Деформирование |
233, 234, 241 |
|
|
||||||||
безмоментное |
|
|
173, |
||||||||
неосесимметрнчное |
|
155, |
159, |
||||||||
191, 203, 234 |
|
|
|
|
|
|
|
|
|||
нестационарное 8, 9, 64, 157 |
|
||||||||||
осесимметричное 13, 158, 234 |
|
||||||||||
Длина полуволны выпучивания |
|
||||||||||
251—253 |
|
139 |
|
|
|
|
|
|
|||
Долговечность |
|
|
|
|
|
|
|||||
Жесткости |
38. 53, 76, 142, 160, 235, |
||||||||||
изгнбные |
|||||||||||
238, 247, 263 |
|
|
|
|
|
|
|
|
|||
кольцевая 238, 240 |
|
|
|
|
|
||||||
мембранно-изгибная 231 |
|
|
|
||||||||
мембранные 38, 53, 142, 160, 235, |
|||||||||||
238, 240, 247, 262 |
|
|
|
|
|
|
|||||
Закон Гука 24 |
15, 25, 29, |
52, |
159, |
||||||||
обобщенный |
|||||||||||
191, 227 |
|
|
|
|
|
|
|
|
|
|
|
Зона |
|
|
|
|
|
|
|
|
|
|
|
краевого эффекта 230, 243 |
|
224, |
|||||||||
начального |
разрушения |
14, |
|||||||||
229, 257 |
|
|
173, 208 |
|
|
|
|
||||
пластическая |
|
|
|
|
|||||||
Изгиб динамический |
|
|
|
|
|
|
|||||
балки 254 |
|
|
|
|
|
|
|
|
|
||
стержня |
153 |
|
|
|
|
|
|
|
|
||
Инерция |
|
12, |
65, |
66, |
68, |
72, |
73. |
||||
вращения |
|
89, 98, 99, 102-104, 106, 112, 121 окружная 75, 76, 102—104
продольная 13, 102, 104, 152, 184 тангенциальная 12, 67, 68, 73, 98, 102, 103, 106, 112
Интеграл свертки 115 Интенсивность касательных напряже ний 170, 201, 204
Колебания |
|
|
|
|
|
|
|
|
|
|
|
|
||
вынужденные 8, 64, 107—109, 111, |
||||||||||||||
121 |
|
|
|
65, |
81, |
89, |
92, |
99, |
|
101, |
||||
нзгибные |
|
|
||||||||||||
104, |
112, |
|
139 |
|
|
|
|
|
|
|
|
|
|
|
крутильные 89, 99 |
|
|
|
|
|
|
||||||||
нестационарные |
138, 139 |
|
|
|
|
|||||||||
осесимметричные |
111, 121 |
|
|
|
||||||||||
параметрические 8, 12, 64, 83, 105, |
||||||||||||||
106, 111—113, |
121, 145, |
185 |
|
|
||||||||||
продольные 89, 99 |
|
65, 67, |
68, |
|||||||||||
собственные |
8, |
12, 64, |
||||||||||||
105, |
107, |
|
108 |
|
|
|
|
|
|
|
|
|
|
|
Композиты |
|
|
|
|
|
|
|
|
|
|
|
|
||
армированные 26, 140, 258 |
|
|
|
|||||||||||
волокнистые |
7, 14, 26, 218 |
|
|
|
||||||||||
слоистые 7, 14, 105, 150, 224—226, |
||||||||||||||
257 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Координаты |
|
|
|
|
|
|
|
|
|
|
|
|||
криволинейные ортогональные 15,19 |
||||||||||||||
начального разрушения |
229, |
230, |
||||||||||||
235 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Коэффициент |
140, |
146, 148—150 |
||||||||||||
армирования |
||||||||||||||
возбуждения 139 |
|
208, |
229, |
230, |
||||||||||
динамичности |
|
207, |
||||||||||||
239 |
|
квадратичной |
формы |
|
21, |
|||||||||
первой |
|
|||||||||||||
23, 50 |
|
|
25, 26, 51 |
|
|
|
|
|
|
|||||
Пуассона |
|
|
|
|
|
|
|
|||||||
сдвига 93 |
|
180, |
|
184, |
187, |
|
189, |
|||||||
Фурье |
158, |
|
|
|||||||||||
191—193, |
|
195, |
198, |
199, |
202, |
203, |
||||||||
206, |
208, |
|
210, |
215, |
218, |
219, |
232, |
|||||||
234 |
239 |
|
251 |
|
|
|
|
|
|
|
|
|
|
|
Краевой эффект 66, 152, 155, 159, |
||||||||||||||
161, 164—166, 170, 182, 183, 200, 243 |
||||||||||||||
Кривизны |
19, 50 |
|
|
|
|
|
|
|
|
|
||||
главные |
|
|
|
|
|
|
|
|
|
|||||
нормальные 21 |
|
|
|
|
|
|
|
|
|
|||||
Критерий |
|
|
|
|
неустойчивости |
|
152, |
|||||||
динамической |
|
|
||||||||||||
171—173, 205, 207, 208, 232 |
|
|
||||||||||||
максимальных |
напряжений |
259 |
||||||||||||
начального разрушения |
263 |
|
|
|||||||||||
прочности |
224, 225, 228 |
|
|
|
||||||||||
композита |
|
|
|
|||||||||||
оболочки 227, 241 |
|
|
|
|
|
|||||||||
слоя 225, 228, 230 |
|
|
|
228, |
||||||||||
тензорно-полиномиальный |
||||||||||||||
259 |
|
|
Мизеса |
170, 171, 206 |
||||||||||
текучести |
|
Материал |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|||
анизотропный 8, 49, 98, 228 |
|
117, |
|||||||||||||||
вязкоупругий |
105, |
|
|
ИЗ, |
116, |
||||||||||||
120, 130 |
|
|
41, 44, |
75, |
76, 86 |
||||||||||||
изотропный |
|
||||||||||||||||
линейно-упругий |
15, 49, |
152, 201, |
|||||||||||||||
209 |
|
|
|
|
14, |
25, |
29, |
51, 53, |
|||||||||
ортотропный |
|||||||||||||||||
104, |
130 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|||
Методы |
|
|
|
|
|
|
|
|
10, |
13, |
105, |
||||||
Бубнова—Галеркнма |
|||||||||||||||||
109, |
122, |
152—154, |
|
173, |
184, |
199, |
|||||||||||
215 |
|
|
|
|
|
148—150 |
|
|
|
|
|
||||||
градиентные |
|
|
|
|
|
|
|||||||||||
конечных |
|
|
10, |
13, 66, |
152, |
155, |
|||||||||||
|
разностей |
||||||||||||||||
|
157, |
173, 199 |
|
|
|
|
|
|
|
|
|
||||||
|
элементов |
10, 266 |
|
|
|
|
|
||||||||||
прямых |
13, 162, 179 |
|
|
|
|
179 |
|||||||||||
пятидиагональной |
|
прогонки |
|
||||||||||||||
Руиге—Кутта |
127, |
|
|
133, |
134, |
|
163, |
||||||||||
179, 187, 188, 222 |
|
|
|
|
|
|
|
|
|
||||||||
Модель |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
||
Амбарцумяна 89 |
12, |
15—19, |
31, |
||||||||||||||
Кирхгофа—ява |
|||||||||||||||||
36, 39, 41, 47—49, |
|
51, 52, |
54, 56, |
||||||||||||||
61, |
|
64, |
67—69, |
88, |
|
113, |
159, |
|
218, |
||||||||
220 |
|
|
|
|
|
|
16, 18 |
|
|
|
|
|
|||||
ломаной линии |
|
|
|
|
|
||||||||||||
прямой |
нормали 38 |
|
|
52, 67, 73, |
|||||||||||||
Тимошенко |
12, |
18, 49, |
|||||||||||||||
89 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Модули |
|
|
|
деформации |
слоя |
|
242 |
||||||||||
поперечной |
|
||||||||||||||||
поперечных |
сдвигов |
|
12, 24, 64, 66, |
||||||||||||||
89, 93, 96, 98, 104, 220, 242 |
|
|
|
||||||||||||||
сдвига |
|
|
|
|
слоя 12, |
84, |
|
219, |
|||||||||
|
в |
|
плоскости |
|
|||||||||||||
|
258 |
|
|
|
|
114 |
|
|
|
|
|
|
|
|
|||
|
длительный |
|
|
|
|
|
|
|
|
||||||||
|
мгновенный |
114 |
|
|
|
|
|
|
|
|
|||||||
|
текущий 259 |
|
|
|
|
|
|
|
|
|
|
||||||
упругости |
|
|
|
|
|
|
|
|
|
|
|
|
|
||||
|
в |
плоскости слоя 64, 66, 87, 94, |
|||||||||||||||
|
98, 258 |
|
|
119—121 |
|
|
|
|
|
||||||||
|
длительный |
|
|
|
|
|
|||||||||||
|
мгновенный |
119—121 |
|
|
|
|
|||||||||||
Момент |
начального |
разрушения |
|
|
|||||||||||||
|
оболочки |
|
14, 228—230, 235, 24. |
||||||||||||||
|
слоя 228, 249 |
|
|
|
|
|
|
|
|
|
|||||||
первого разрушения слоя 224, |
|
||||||||||||||||
225, 227, 231, 240, 250 |
|
|
|
|
|
||||||||||||
Моменты |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|||
дополнительные 47 |
|
|
|
|
|
|
|
|
|||||||||
изгибающие 34, 107 |
|
|
|
|
|
|
|
||||||||||
крутящие 34 |
|
|
|
|
|
|
|
|
|
|
|
||||||
массовых |
сил 41, 47, 53, 55 |
|
|
||||||||||||||
обобщенные 38, 39, 41, 52, 55 |
|
поверхностных |
сил 41, 47, 53, 54, |
||
60 |
14, |
141, |
142, 209, 210, 229, |
Монослой |
|||
234, 259, 260, 263 |
|
Нагружение |
|
|
|
|
|
|
|
|
|
|
|
|
вибрационное 10, 11, 106, 145, 151 |
||||||||||||
импульсное |
10, 13, 108, 156, 185 |
|||||||||||
квазистатнческое 156 |
|
|
|
|
||||||||
комбинированное |
динамическое |
|||||||||||
216, 217 |
|
|
|
|
|
|
|
|
|
|
|
|
осевое статическое 215, 217 |
|
|
||||||||||
предварительное статическое 214 |
||||||||||||
совместное динамическое 210, 212, |
||||||||||||
214 |
|
|
|
|
|
|
|
|
|
|
|
|
Нагрузки |
|
|
|
13, |
|
105, |
|
111, |
139, |
|||
вибрационные |
|
|
||||||||||
184 |
|
|
|
|
|
|
|
|
|
|
|
|
импульсные 9, 11, 14, 184 |
|
|
|
|||||||||
консервативные 47 |
|
|
|
|
|
|
|
|||||
критические |
|
227, |
229, |
230, |
||||||||
динамические |
||||||||||||
232, 240 |
|
12, 83, 86—88, 106, |
||||||||||
статические |
||||||||||||
159, 215, 218 |
|
|
|
|
225, |
228, |
||||||
начального |
разрушения |
|
||||||||||
229, 238, 258 |
|
|
|
|
|
|
|
|
||||
поверхностные 41, 53, 54, 246 |
|
|||||||||||
предельные |
14, 257, 258 |
|
|
|
|
|||||||
следящие 47, 70 |
|
|
|
|
|
|
|
|||||
ударные 9, 11, 158 |
|
|
|
|
|
|
||||||
Надежность 7, 9, 226 |
|
|
|
|
|
|
|
|||||
Напряжения |
|
|
|
|
|
|
|
|
|
|
|
|
безмоментные 137 |
|
|
|
|
|
|
|
|||||
касательные |
105, 114, 258 |
|
138, |
|||||||||
кольцевое |
|
|
(окружное) |
|
137, |
|||||||
235, 240, 243 |
|
|
|
|
|
|
|
|
||||
межслойные 14, 224, 226, 241, 253, |
||||||||||||
256, 257 |
|
|
|
|
|
|
|
|
|
|
|
|
мембранные 235 |
|
|
|
|
|
|
|
|||||
начальные |
17, 45, 46 |
|
|
|
|
|||||||
обобщенные 27, 28 |
|
|
|
|
|
|
||||||
осевое 137, 163, 243 |
|
|
241—244, |
|||||||||
поперечные |
14, |
|
224, |
|
||||||||
247—254, 256, 257 |
|
89, |
92, |
242, |
||||||||
касательные |
16, |
|||||||||||
244, 250—252, 256 |
|
|
|
|
||||||||
нормальное 242, 250, 251, 257 |
||||||||||||
продольное 235 |
|
|
|
|
|
|
|
|||||
Несовершенства |
13, |
|
17, |
45, |
46, |
65, |
||||||
начальные |
|
10, |
|
|||||||||
67, |
106, |
126, |
128, |
|
154, |
157, |
158, |
|||||
167, |
168, |
|
181, |
190, |
191, |
196, |
198, |
|||||
199, 203, |
|
204, |
208—212, |
214, 216, |
||||||||
232—234, |
|
242, |
248, |
251, |
254, |
260 |
||||||
стохастические |
158, 226 |
|
|
|
||||||||
Оболочки |
|
|
|
18, |
|
19, |
24, |
67, |
68, |
|||
анизотропные |
|
|||||||||||
81 |
|
|
|
|
|
|
|
|
|
|
|
|
биметаллические |
16 |
|
|
|
|
|
||||||
боропластиковые |
106, 142, 149 |
|
||||||||||
весьма |
пологие |
16, 19, 44 |
|
109, |
||||||||
вязкоупругие |
12, |
105, |
106, |
|||||||||
113, |
114, |
117, |
130, |
133, |
134, |
135, |
||||||
145 |
|
|
|
|
|
|
|
|
|
|
|
|
двухслойные 66, 69, 150, 231 |
63, |
|||||||||||
изотропные |
|
9, |
18, |
19, 41, |
49, |
|||||||
66, |
69, |
89, |
98, |
103, |
104, |
120, |
123, |
|||||
155, 232 |
|
|
|
|
|
|
|
|
16, 63, |
|||
конструктивно-ортотропные |
||||||||||||
67 |
|
|
|
|
|
|
11, |
14, |
|
16—19, |
||
многослойные |
|
|
||||||||||
66-68, 106, 139, 142, 144, 145, |
||||||||||||
148, 226, |
227, 235, |
239, |
242, |
256, |
||||||||
260, 262, 263 |
59, |
152, |
154—156, |
|||||||||
несовершенные |
||||||||||||
226, 254, 258, 263 |
|
|
|
|
|
|||||||
ортотропные 9, 11—13, 15—17, 38, |
||||||||||||
41, 42, |
44, 48, 49, |
52, |
55, 56, |
59, |
||||||||
60, 62, 64, 66—69, 83, 87—89, 96, |
||||||||||||
98, |
103, |
105, |
136, |
141, |
142, |
152, |
||||||
153, 155, 159 |
|
|
|
|
|
155 |
||||||
перекрестно |
|
армированные |
||||||||||
пологие |
18, 41, 45, 68, 242 |
|
|
|||||||||
регулярного |
|
строения |
17, 18, 66 |
|||||||||
стеклопластнковые 8, 9, 95, 106, |
||||||||||||
142, 158 |
|
|
16, 19, 66, 69, 89 |
|
||||||||
трехслойные |
|
|||||||||||
углепластнковые 78, 81, 99, 102, |
||||||||||||
106, |
142, |
144, |
150, |
163, |
199, |
209, |
||||||
210, |
215, |
218, |
224, |
229, |
235, |
238, |
||||||
248, 258 |
|
|
|
|
|
|
|
|
|
|
Ограничения физические 8, 13, 105, |
||||
145—151 |
|
|
||
Операторы |
|
162, 163, 246 |
||
дифференциальные |
||||
интегральные 114, 117, 130 |
||||
Оптимальное |
проектирование 8, 13, |
|||
105, 106, 145, 147—150, 214 |
||||
Осевое |
(продольное) |
динамическое |
||
сжатие |
153, |
156, 158, |
189, 191—193, |
|
195, |
199, 201, 203, 204, 207, 209, 210, |
212, 215—218, 222, 224, 229, 230, 238, 242, 247, 248, 251—254, 256, 258, 260, 262
Панели пологие 108
цилиндрические 9, 108, 153 Параметрические колебания
нелинейные 107, 108, 109, 121—123, 125, 128—130, 133 пластинок 105, 106 стержней 105, 106, 118, 128 эксперименты 106, 109, 139
Параметры Ламе 21