Calculation of the collapse load of an axially compressed laminated composite stringer-stiffened curved panel-An engineering approach

Composite Structures

Volumn 83, Issue 4, 2008, Pages 341-353

  Pevzner, P ^a   Abramovich, H ^a   Weller, T ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

Buckling load; Collapse; Effective width; Laminated composite curved panel; Stringer stiffened panel

Indexed keywords

BENDING (DEFORMATION); BUCKLING; LAMINATED COMPOSITES; STIFFNESS; STRUCTURAL ANALYSIS; STRUCTURAL LOADS; TORSIONAL STRESS;

BUCKLING LOAD; EFFECTIVE WIDTH; LAMINATED COMPOSITE CURVED PANEL; STRINGER-STIFFENED PANEL;

STRUCTURAL PANELS;

BENDING; BUCKLING; COMPOSITE; FINITE ELEMENT ANALYSIS; LAMINATE; STIFFNESS;

EID: 38849153432     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2007.05.001     Document Type: Article

References (21)

1. von Kármán T., Sechler E.E., and Donnel L.H. The strength of thin plates in compression. ASME Appl Mech Trans 54 (1932) 53-57
2. Sechler EE. The ultimate strength of flat sheets in compression, GALCIT Publication 27, Guggenheim Aeronautics Laboratory, California Institute of Technology, Pasadena; 1933.
3. Cox HL. Buckling of thin plates in compression, Aeronautical Research Committee, R.&M. No. 1554; 1933.
4. Lahde-Wagner. Versuche zur Ermittlung der mittragenden Breite von verbeulten Blechen. Luftfahrt-Forchung 13 (1936) 214-223
5. Sechler E.E. Stress distribution in stiffened panels under compression. J Aeronaut Sci 4 8 (1937) 320-323
6. Marguerre K. Die mittragende Breite der gedrückten Platte. Luftfahrt-Forchung 14 3 (1937) 121-128 Translated as the apparent width of the plate in compression, NACA TM 833; 1937
7. Dickinson H.B., and Fischel J.R. Measurement of stiffener stresses and effective width in stiffened panels. J Aeronaut Sci 6 6 (1939) 249-254
8. Hoff N.J. Instability of monocoque structures in pure bending. J Roy Aeronaut Soc 42 (1938) 291-346
9. Sechler E.E., and Dunn L.G. Airplane structural analysis and design (1942), John Wiley & Sons, New York p. 201-34
10. Singer J., Arbocz J., and Weller T. Buckling experiments, experimental methods in buckling of thin walled structures. Basic concepts, columns, beams and plates vol. 1 (1998), John Wiley & Sons, Inc., New York
11. Sechler E.E., and Dunn L.G. Airplane structural analysis and design (1963), Dover Publications, Inc.
12. Sechler E.E. Elasticity in engineering (1952), John Wiley & Sons, Inc.
13. Calcote L.R. The analysis of laminated composite structures (1969), Van Nostrand Company
14. Viswanathan AV, Tamekuni M. Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads, Report, NASA-CR-2216, 88 pp, March 1973.
15. Viswanathan AV, Tamekuni M, Baker LL. Elastic stability of laminated flat and curved long rectangular plates subjected to combined inplane loads, Report, NASA CR-2330, 65 pp, July 1973.
16. Viswanathan AV, Tamekuni M. Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads, Report, 88 pp, September 1973.
17. Leissa AW. Buckling of laminated composite plates and shell panels, final report for the period November 1980-January 1985, Report, AFWAL-TR-85-3069, 454 pp, June 1985.
18. Ashton J.E., and Whitney J.M. Theory of laminated plates (1970), Technomic Publishing Co., Inc.
19. Timoshenko S.P., and Gere J.M. Theory of elastic stability. International ed. (1963), Mcgraw-Hill Book Company
20. Timoshenko S.P. Strength of materials. Part I. 3d ed. (1956), D. Van Nostrand Company, Inc., Princeton, NJ
21. Timoshenko S.P. Strength of materials. Part II. 3d ed. (1955), D. Van Nostrand Company, Inc., Princeton, NJ