The constant-moment plate-bending element

The Journal of Strain Analysis for Engineering Design

Volumn 6, Issue 1, 1971, Pages 20-24

  Morley, L S D ^a  

^a Royal Aircraft Establishment   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

PLATES--STRESSES;

EID: 0015000553     PISSN: 03093247     EISSN: 20413130     Source Type: Journal    
DOI: 10.1243/03093247V061020     Document Type: Article

References (9)

1. Bazeley G. P., Cheung Y. K., Irons B. M., Zienkiewicz O. C. ‘Triangular elements in plate bending’conforming and non-conforming solutions’, Matrix Meth. struct. Mech. 1966 AFFDL-TR-66—80, 547.
2. Herrmann L. R. ‘Finite-element bending analysis for plates’, J. Engng Mech. Div. Am. Soc. civ. Engrs 1967 93, EM5.
3. Allman D. J. ‘Triangular finite elements for plate bending with constant and linearly varying bending moments’, IUTAM Symp. High-speed Computing Elastic Structures 1970 ( Liège).
4. Fraeijs De Veubeke B., Sander G. ‘An equilibrium model for plate bending’, Int. J. Solids Structs 1968 4, 447.
5. Herrmann L. R., Campbell D. M. ‘A finite element analysis for thin shells’, A.I.A.A. fl 1968 6, 1842.
6. Kawai T. ‘Finite element analysis of shell structures in Japan’, Japan-U.S. Semin. Matrix Meth struct. Analysis Des. 1969 ( Tokyo).
7. Fujino T. ‘Analyses of hydrodynamic and plate structure problems by finite element methods’, ibid.
8. Irons B. M. ‘A frontal solution program for finite element analysis’, Int. J. Num. Meth. in Engng 1970 2, 5.
9. Timoshenko S., Woinowsky-Krieger S. Theory of plates and shells 1959 ( McGraw-Hill Book Co. Inc., New York and London).