journal article·2017-05

Wave transmission characteristics for higher-order sandwich panel with flexible core using time-domain spectral element method

B Raja Sekhar, S Gopalakrishnan, MVVS Murthy

Publisher page

Abstract

A new time-domain spectral element with nine degrees of freedom per node is formulated based on higher-order sandwich panel theory, incorporating the flexible behaviour of the core with composite face sheets. Static, free vibrations and wave propagation analysis are carried out using the formulated element. Results obtained using this element are compared with those available in the literature and with commercial finite element codes. The fast convergence of the spectral element method is demonstrated by solving the high-frequency wave propagation problem. A method of computing the wave characteristics, namely wavenumbers and group velocities, in a higher-order sandwich panel is developed using the formulated element. The effect of core damping is studied in detail with different core types, which can be used effectively in sandwich beam design.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Composite Structure Analysis and Optimization · Acoustic Wave Phenomena Research · Vibration and Dynamic Analysis

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Aerospace Engineering, Indian Institute of Science, India

Structures Group, ISRO Satellite Centre, India

References (29)

Show source-provided references
1. Zenkert D · 1995
2. 10.2174/221279761080101002910.2174/2212797610801010029 ↗
3. 10.1061/(ASCE)0733-9399(1992)118:5(1026)10.1061/(ASCE)0733-9399(1992)118:5(1026) ↗
4. 10.1061/(ASCE)0733-9399(1996)122:11(1069)10.1061/(ASCE)0733-9399(1996)122:11(1069) ↗
5. 10.1016/j.ijimpeng.2006.05.00710.1016/j.ijimpeng.2006.05.007 ↗
6. 10.1115/1.400555010.1115/1.4005550 ↗
7. 10.1007/s00419-012-0673-x10.1007/s00419-012-0673-x ↗
8. 10.1115/1.402361910.1115/1.4023619 ↗
9. 10.2514/2.99110.2514/2.991 ↗
10. 10.1002/cnm.108610.1002/cnm.1086 ↗
11. 10.1016/j.jsv.2006.07.03110.1016/j.jsv.2006.07.031 ↗
12. 10.1007/978-1-4612-1832-610.1007/978-1-4612-1832-6 ↗
13. Gopalakrishnan S · 2007
14. 10.1016/j.jsv.2003.11.02610.1016/j.jsv.2003.11.026 ↗
15. Murthy MVVS · J Aerosp Sci Technol · 2011 · 63 · 1
16. 10.1016/0021-9991(84)90128-110.1016/0021-9991(84)90128-1 ↗
17. 10.1002/nme.162038080710.1002/nme.1620380807 ↗
18. Boyd JP · 2001
19. 10.1007/978-3-540-30728-010.1007/978-3-540-30728-0 ↗
20. 10.1016/j.finel.2015.06.00710.1016/j.finel.2015.06.007 ↗
21. 10.1016/S0263-8223(01)00130-110.1016/S0263-8223(01)00130-1 ↗
22. 10.2514/1.J05373610.2514/1.J053736 ↗
23. 10.1177/1045389X990100010610.1177/1045389X9901000106 ↗
24. 10.1121/1.41965210.1121/1.419652 ↗
25. Brillouin L · 1953
26. 10.1016/S0022-460X(74)80108-210.1016/S0022-460X(74)80108-2 ↗
27. Ichchou MN · Finite Elem Anal Des · 2007 · 305 · 931
28. 10.1016/j.ijmecsci.2015.03.02010.1016/j.ijmecsci.2015.03.020 ↗
29. Reddy JN · 1997