Buckling analysis of anisotropic variable-curvature panels and shells

Composite Structures

Volumn 43, Issue 4, 1998, Pages 321-329

  Jaunky, Navin ^a   Knight Jr , Norman F ^a,c   Ambur, Damodar R ^b  

^a Old Dominion University ^*  (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c MRJ Technology Solutions   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; SHEAR DEFORMATION; SHELLS (STRUCTURES); STRUCTURAL PANELS;

BEZIER FUNCTIONS; RITZ FUNCTIONS; VARIABLE CURVATURE PANELS;

STRUCTURAL ANALYSIS;

EID: 0032266523     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(98)00118-4     Document Type: Article

References (21)

1. [1] Marguerre K. Stability of the Cylindrical Shell of Variable Curvature. NASA TM 1302, 1951.
2. [2] Chen YN, Kempner J, Large deflection of an axialiy compressed oval cylindrical shell. Proceeding of the 9th International Congress on Applied Mechanics, Munich, Germany, 1964, Berlin: Springer, 1965:299-305.
3. [3] Sheinman I, Frier M, Buckling analysis of laminated cylindrical shells with arbitrary noncircular cross section. AIAA Journal 1994;32(3):648-661.
4. [4] Meyers CA. An analytical and experimental investigation of elliptical composite cylinders. Virginia Polytechnic Institute and State University, Ph.D. Dissertation, Engineering Science and Mechanics Department, April 1996.
5. [5] Boyd DE. Analysis of open non-circular cylindrical shells. AIAA Journal 1969;7(3):563-565.
6. [6] Kurt CE, Boyd DE. Free vibration of non-circular cylindrical shell segments. AIAA Journal 1971;9(2):239-244.
7. [7] Culberson LD, Boyd DE. Free vibrations of freely supported oval cylinders. AIAA Journal 1971;9(8):1474-1480.
8. [8] Elsbernd GF, Leissa AW. The vibrations of non-circular shells with initial stresses. Journal of Sound and Vibration 1973;29(3):309-329.
9. [9] Chen YN. Kempner J. Modal method for free vibration of oval cylindrical shells with simply supported or clamped ends. ASME Journal of Applied Mechanics 1978;45(1):142-148.
10. [10] Koumousis VK, Armenakas AE. Free vibration of non-circular panels with simply supported curved edges. ASCE Journal of Engineering Mechanics 1984;110(5):810-827.
11. [11] Koumousis VK, Armenakas AE. Free vibration of simply supported cylindrical shells. AIAA Journal 1983;21(7):1017-1027.
12. [12] Irie T, Yamada G, Kaneko Y. Free vibration of a conical shell with variable thickness. Journal of Sound and Vibration 1982;82(1):83-94.
13. [13] Singh AV. On vibrations of shells of revolution using bezier polynomials. ASME Journal of Pressure Vessel Technology 1991;113:579-584.
14. [14] Kumar V, Singh AV. Vibration analysis of non-circular cylindrical shells using Bezier functions. Journal of Sound and Vibration 1993;161(2):333-354.
15. [15] Kumar V, Singh AV. Vibration of composite non-circular cylindrical shells. ASME Journal of Vibration and Acoustics 1995;117:470-476.
16. [16] Kumar V, Singh AV. Vibration of fiber-reinforced laminated deep shells. ASME Journal of Pressure Vessel Technology 1996;118:407-414.
17. [17] Sanders Jr JL, An improved first approximation theory for thin shells. NASA Report R-24, 1959.
18. [18] Koiter WT. A consistent first approximation in general theory of thin elastic shells, the theory of thin elastic shells. Proceedings IUTAM Symposium, Delft, 1959, Amsterdam, the Netherlands. Amsterdam: North-Holland, 1960:12-33.
19. [19] Love AEH. Treatise on the Mathematical Theory of Elasticity. 4th ed, New York: Dover, 1927.
20. [20] Loo TT. An extension of Donnell's equation for circular cylindrical shell. Journal of Aeronautical Sciences 1957;24:390-391.
21. [21] Brogan FA, Rankin CC, Cabiness HD, Loden WA. STAGS user's manual. Lockheed Martin Missiles and Space, Report LMMSC P032594, version 2.3, 1996.