Adhesively bonded single lap joint of composites
Uniones adhesivas de traslape simple de compuestos
dc.creator | Alvarado Prieto, Peter | |
dc.date | 2013-09-01 | |
dc.date.accessioned | 2021-06-17T12:57:07Z | |
dc.date.available | 2021-06-17T12:57:07Z | |
dc.identifier | https://publicacionesfac.com/index.php/cienciaypoderaereo/article/view/5 | |
dc.identifier | 10.18667/cienciaypoderaereo.5 | |
dc.identifier.uri | https://hdl.handle.net/20.500.12963/70 | |
dc.description | A study of single lap joints of composite materials with and without attachments is presented. Failure of this type of joint is caused by the high peel stress in a perpendicular direction presented in the geometric singularity. It is shown that the joint strength is affected by factors such as surface preparation, the adhesive curing process and cleaning. The two configurations, with and without attachments, are compared. It is shown that the single lap joint with attachment has a higher strength than the joint without attachments when no fillet is left on the geometrical singularity. However, because of the low increase in joint strength and the complexity of manufacturing, the choice of type of joint is left to the manufacturer's judgment. | eng |
dc.description | El siguiente artículo muestra un estudio de uniones de traslape simple de materiales compuestos, con y sin modificación. La falla de este tipo de uniones es causada por el alto esfuerzo de despegue en dirección perpendicular a la aplicación de la fuerza presentado en la singularidad geométrica. Se muestra que la resistencia de la unión es afectada por factores como la preparación de la superficie, el proceso de curado del adhesivo, y la limpieza. Ambas configuraciones, con y sin modificación, son comparadas. Se muestra que la unión de traslape simple modificada, tiene una mayor resistencia que sin modificación cuando se remueve el exceso de adhesivo en la singularidad geométrica. Sin embargo, el bajo incremento en la resistencia de la unión y la complejidad para manufactura, deja a consideración del fabricante la decisión respecto a qué tipo de unión usar. | spa |
dc.format | application/pdf | |
dc.format | text/html | |
dc.language | eng | |
dc.publisher | Escuela de Postgrados de la Fuerza Aérea Colombiana | spa |
dc.relation | https://publicacionesfac.com/index.php/cienciaypoderaereo/article/view/5/6 | |
dc.relation | https://publicacionesfac.com/index.php/cienciaypoderaereo/article/view/5/107 | |
dc.relation | /*ref*/Adams, R (1989). Strength Predictions for Lap Joints, Especially with Composite Adherends: A review. Journal of adhesion,30, pp.219-242. https://doi.org/10.1080/00218468908048207 | |
dc.relation | /*ref*/Adams, R. D, Comyn, J. and Wake, W. C. (1997) Structural Adhesive Joints in Engineering, 2nd ed. London; New York: Chapman &Hall. | |
dc.relation | /*ref*/Albericci, P. (1983). Aerospace Applications in Durability of Structural adhesives. Edited by Kinloch, A. J., Applied Science Publishers. | |
dc.relation | /*ref*/ASTM D5868 (2008). Standard Test Method for Lap Shear Adhesion for Fiber Reinforced Plastic (FRP) bonding. AST Mannual book of standards. | |
dc.relation | /*ref*/Cagle, C. V. (1968). Adhesive Bonding: Techniques and Applications. New York: McGraw-Hill. | |
dc.relation | /*ref*/Chung, D. (2010). Composite Materials: Science and Applications. New York: Springer. https://doi.org/10.1007/978-1-84882-831-5 | |
dc.relation | /*ref*/Coates, C. W., & Armanios, E. A. (2000). An Assessment of Nested Overlap and Transverse Interfacial Layer in Co-Cured Composite Single Lap Joints. American Society for Composites. Dayton, OH. | |
dc.relation | /*ref*/Flinn, B., Ohuchi, F., Phariss, M., Satterwhite, J., Au-bin, J., & Keenen, C. (2010). Improving Adhesive Bonding of Composites through Surface Characterization, The Joint Advanced Materials and Structures Center of Excellence, CECAM, and AMTAS, University of Washington in: http://depts.washington.edu/amtas/ev-ents/ jams_/21.Flinn.pdf | |
dc.relation | /*ref*/Gordon, K. (2005). Load Transfer in Hybrid (Bonded/Bolted) Composite Single-Lap Joints. Composite Structures, 69, pp.35-43. https://doi.org/10.1016/j.compstruct.2004.04.016 | |
dc.relation | /*ref*/Gordon, K. (2006). Quasi-Static Strength and Fatigue Life of Hybrid (bonded/bolted) composite single-lap joints. Composite Structures, 72:119-129. https://doi.org/10.1016/j.compstruct.2004.11.002 | |
dc.relation | /*ref*/Guess, T. R., Reedy, E. D.,.& Stavig, M. E. (1995). Mechanical properties of hysol ea-9394 structural adhesive. Technical Report SAND95-0229, Sandia National Laboratories. https://doi.org/10.2172/32591 | |
dc.relation | /*ref*/Kinloch, A. J. (1997). Adhesives in Engineering, Proceedings of the Institution of Mechanical Engineers. Part G, Journal of Aerospace Engineering, 211, pp.307-335. https://doi.org/10.1243/0954410971532703 | |
dc.relation | /*ref*/Ko, W, (1985). Stress Concentration Factor Around A Small Circular Hole In The Himat Composite Plate. NASA Technical memorandum 86038. | |
dc.relation | /*ref*/Kuhbander, R. (1994). Characterization of ea9394 Adhesive for Repair Applications. Technical Report WL-TR-92-4069, University of Dayton. | |
dc.relation | /*ref*/Matthews, F.L., & Tester, T.T. (1985). The Influence of Stacking Sequence on the Strength of bonded CFRP single lap joints. International Journal of Adhesion and Adhesives, 5(1), pp.13-18. https://doi.org/10.1016/0143-7496(85)90040-5 | |
dc.relation | /*ref*/Mays, G. C. and Hutchinson, A. R. (1992). Adhesives in Civil Engineering, Cambridge University Press, Cambridge. https://doi.org/10.1017/CBO9780511529597 | |
dc.relation | /*ref*/Qian, H. (2008). A Study of Failure in Bonded Lap Joints Using Fracture Mechanics. PhD thesis, Purdue University. | |
dc.relation | /*ref*/Qing, Z., & Sun, C. T, (2001). Novel Design of a Bonded Lap Joint. AIAA Journal, 39(10), pp. 1991-1996. https://doi.org/10.2514/2.1191 | |
dc.relation | /*ref*/Renton, W. J., & Vinson, J. R. (1975). The Efficient Design of Adhesive Bonded Joints, Journal of Adhesion, 7, 1975, pp.175-193. doi:10.1080/00218467508075049 https://doi.org/10.1080/00218467508075049 | |
dc.relation | /*ref*/Roh, H. S.(2011). Repairs of Composite Structures. Ph.D. thesis, Purdue University. | |
dc.relation | /*ref*/Sadek, M. M. (1987), Industrial Applications of Adhesive https://doi.org/10.1007/978-94-009-3419-1 | |
dc.relation | /*ref*/Bonding. London; New York: Elsevier Applied Science. | |
dc.relation | /*ref*/Sun, C.T. (2004). Design of Efficient Bonded Joints for Thin Walled Composites Structures. Proceedings for The Joint American Society Of Composites / American Society for Testing and Materials Committee D30 - Nineteenth Technical Conference, Atlanta, GA. | |
dc.relation | /*ref*/Tomblin, J.S., Yang, C. & Harter, P. (2001). Investigation of thick bondline adhesive joints. Final Report DOT/FAA/AR 01/33, Wichita State University. | |
dc.relation | /*ref*/Turaga, U.V.R.S. & Sun, C. T. (2003). An investigation of Adhesively single-lap joints with attachments. 44rd AIAA/ASME/ASCE/AHS/ACS Structures, Structural Dynamics, and Materials Conference. Norfolk, Va. https://doi.org/10.2514/6.2003-1957 | |
dc.relation | /*ref*/Turaga, U.V.R.S. & Sun, C. T. (2008). An Improved Design for Metallic and Composite Single-Lap Joints. AIAA Journal of Aircraft, 45(2), pp. 440-447. https://doi.org/10.2514/1.28934 | |
dc.relation | /*ref*/Zhuguo, Z., Yingchun, Z., & Xupo, O. (2011). Study on Key Certification Issues of Composite Airframe Structures for Commercial Transport Airplane. Procedia Engineering, 17, pp. 247-257. https://doi.org/10.1016/j.proeng.2011.10.026 | |
dc.source | Ciencia y Poder Aéreo; Vol. 8 No. 1 (2013): Enero - Diciembre; 33-41 | eng |
dc.source | Ciencia y Poder Aéreo; Vol. 8 Núm. 1 (2013): Enero - Diciembre; 33-41 | spa |
dc.source | Ciencia y Poder Aéreo; v. 8 n. 1 (2013): Enero - Diciembre; 33-41 | por |
dc.source | 2389-9468 | |
dc.source | 1909-7050 | |
dc.subject | Adherent | eng |
dc.subject | adhesive | eng |
dc.subject | bond line | eng |
dc.subject | composite | eng |
dc.subject | joints | eng |
dc.subject | Adherent | spa |
dc.subject | adhesive | spa |
dc.subject | bond line | spa |
dc.subject | composite | spa |
dc.subject | joints | spa |
dc.title | Adhesively bonded single lap joint of composites | eng |
dc.title | Uniones adhesivas de traslape simple de compuestos | spa |
dc.type | info:eu-repo/semantics/article | |
dc.type | info:eu-repo/semantics/publishedVersion |
Files in this item
Files | Size | Format | View |
---|---|---|---|
There are no files associated with this item. |
This item appears in the following Collection(s)
-
Revista Ciencia y Poder Aéreo
Cosecha OJS