Supersonic flutter prediction of functionally graded cylindrical shells

Composite Structures

Volumn 83, Issue 4, 2008, Pages 391-398

  Haddadpour, H ^a   Mahmoudkhani, S ^a   Navazi, H M ^a  

^a SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

Cylindrical shell; Flutter; Functionally graded; In plane boundary conditions; Supersonic

Indexed keywords

BOUNDARY CONDITIONS; CYLINDERS (SHAPES); FLUTTER (AERODYNAMICS); FUNCTIONALLY GRADED MATERIALS; GALERKIN METHODS; SUPERSONIC AERODYNAMICS; TEMPERATURE DISTRIBUTION;

AEROELASTIC EQUATIONS; IN-PLANE BOUNDARY CONDITIONS; SUPERSONIC FLUTTER ANALYSIS;

SHELLS (STRUCTURES);

MATHEMATICAL ANALYSIS; PRESSURE; STRUCTURAL ANALYSIS; TEMPERATURE;

EID: 38849181525     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2007.05.011     Document Type: Article

References (22)

1. Loy C.T., Lam K.Y., and Reddy J.N. Vibration of functionally graded cylindrical shells. Int J Mech Sci 41 (1999) 309-324
2. Pradhan S.C., Loy C.T., Lam K.Y., and Reddy J.N. Vibration characteristics of functionally graded cylindrical shells under various boundary conditions. Appl Acoust 61 (2000) 111-129
3. Kadoli R., and Ganesan N. Buckling and free vibration analysis of functionally graded cylindrical shells subjected to a temperature-specified boundary condition. J Sound Vib 289 (2006) 450-480
4. Shahsiah R., and Eslami M.R. Thermal buckling of functionally graded cylindrical shell. J Therm Stresses 26 (2003) 277-294
5. Shen H.-S. Postbuckling analysis of pressure-loaded functionally graded cylindrical shells in thermal environments. Eng Struct 25 (2003) 487-497
6. Shen H.-S. Thermal postbuckling behavior of functionally graded cylindrical shells with temperature-dependent properties. Int J Solids Struct 41 (2004) 1961-1974
7. Shen H.-S. Postbuckling of axially loaded FGM hybrid cylindrical shells in thermal environments. Compos Sci Technol 65 (2005) 1675-1690
8. Shen H.-S., and Noda N. Postbuckling of FGM cylindrical shells under combined axial and radial mechanical loads in thermal environments. Int J Solids Struct 42 (2005) 4641-4662
9. Wu L., Jiang Z., and Liu J. Thermoelastic stability of functionally graded cylindrical shells. Compos Struct 70 (2005) 60-68
10. Olson M.D., and Fung Y.C. Comparing theory and experiment for the supersonic flutter of circular cylindrical shells. AIAA J 5 (1967) 1849-1856
11. Barr G.W., and Stearman R.O. Aeroelastic stability characteristics of cylindrical shells considering imperfections and edge constraint. AIAA J 7 5 (1968) 912-919
12. Carter L.L., and Stearman R.O. Some aspects of cylindrical shell panel flutter. AIAA J 6 1 (1968) 37-43
13. Ganapathi M., Varadan T.K., and Jijen J. Field-consistent element applied to flutter analysis of circular cylindrical shells. J Sound Vib 171 (1994) 509-527
14. Pidaparti R.M.V., and Yang H.T.Y. Supersonic flutter analysis of composite plates and shells. AIAA J 31 6 (1993) 1109-1117
15. Prakash T., and Ganapathi M. Supersonic flutter characteristics of functionally graded flat panels including thermal effects. J Compos Struct 72 1 (2006) 10-18
16. Navazi H.M., and Haddadpour H. Aero-thermoelastic stability of functionally graded plates. J Compos Struct 80 (2007) 580-587
17. Haddadpour H., Navazi H.M., and Shadmehri F. Nonlinear oscillations of a fluttering functionally graded plate. J Compos Struct 79 (2007) 242-250
18. Haddadpour H, Mahmoudkhani S, Navazi HM, Free vibration analysis of functionally graded cylindrical shells including thermal effects. J Thin Walled Struct, in press, doi:10.1016/j.tws.2007.04.007.
19. Reddy J.N., and Chin C.D. Thermomechanical analysis of functionally graded cylinders and plates. J Therm Stresses 21 (1998) 593-626
20. Touloukian Y.S. Thermophysical properties of high temperature solid materials (1967), McMillan, NewYork
21. Krumhaar H. The accuracy of linear piston theory when applied to cylindrical shells. AIAA J 1 (1963) 1448-1449
22. Amabili M., and Pellicano F. Multimode approach to nonlinear supersonic flutter of imperfect circular cylindrical shells. J Appl Mech 69 (2002) 117-129