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BUCKLING OF SYMMETRICALLY LAMINATED THIN RECTANGULAR COMPOSITE PLATES

Year 2017, Volume: 19 Issue: 56, 553 - 568, 01.05.2017

Abstract

Critical buckling loads of symmetrically laminated thin rectangular composite plates were examined in this study. Rayleigh-Ritz Method was used to solve the governing energy equations based on Classical Laminated Plate Theory. Critical buckling loads of 24 differently laminated simply supported plates with in-plane force at the edge were calculated parametrically for 12 different aspect ratios. Results were compared with those obtained by ANSYS software package based on Finite Element Method, which seem to be approximate. The aim of this study was mainly to find the most suitable lamination type of plates. Nondimensionally tabulated results were given for practical use at the preliminary structural design stage of composite vessels. Thus, it is expected to save material, labor, time and test costs during production stage

References

  • Reuben, R.L. 1994. Materials in Marine Technology. Springer- Verlag, London Limited, UK.
  • Shenoi, R.A., Wellicome, J.F. 1993. Composite Materials in Maritime Structures, (Fundamental Cambridge University Pres, NY. Aspects),
  • Shenoi, R.A., Wellicome, J.F. 1993. Composite Materials in Maritime Structures, Volume-II (Practical Considerations), University Pres, NY.
  • Mouritz, A.P., Gellert, E., Burchill, P., Challis K., 2001. Review of Advanced Composite Structures for Naval Ships and Submarines, Composite Structures, Cilt. 53, s..21-41.DOI:10.1016/S0263- 8223(00)00175-6
  • Savcı, M., 1987. Gemi Yapısında Levhalar ve Silindirik Kabuklar, İ.T.Ü. Gemi İnş. ve Deniz Bil. Fak, İstanbul.
  • Lekhnitskii, S.G.1968. Anisotropic Plates, NewYork. Breach, Malzemeler, İ.T.Ü. Sayı:1420,
  • Powell, P.C., 1994. Engineering with fibre-polymer laminates, Chapman & Hall, London, UK.
  • Mallick. P. K., 1997. Composites engineering handbook, Marcel Dekker Inc., NY.
  • ASM Handbook, 2001. Volume 21, Composites, ASM International.
  • Harper, C.A., 2002. Handbook of plastics, composites, McGraw-Hill, NY. and
  • Ambartsumyan, S.A, 1970. Theory of Anisotropic Plates, Technomic Publishing, Co., Wesport Conn.
  • Baharlou, B., Leissa A.W., 1987. Vibration Generally Laminated Composite Plates conditions, Int. J. Mech. Sci. Vol. 29, No. 8, pp. 545-555.DOI: 10.1016/0020-7403(87)90026-9
  • Lakshminarayana, L., Kumar, Krishna Mohana Rao G., 2012. Buckling isotropic quasi- symmetrically laminated rectangular composite plates with an elliptical/circular cutout subjected to linearly varying in-plane loading using FEM, International Journal Of Mechanics, Issue 1, Volume 6.
  • Hu, H., Badir, A., Abatan, A., 2003. Buckling graphite/epoxy composite plate under parabolic variation of axial loads, Int. J. Mech. Sci. 45, 1135– 1147.DOI:10.1016/j.ijmecsci.200 3.08.003 of a
  • Darvizeh, M., Darvizeh, A., Ansari, R., Sharma, C.B., 2004. Buckling analysis of generally laminated composite plates (generalized differential versus Rayleigh–Ritz method), Composite Structures 63, 69– 74.DOI: 8223(03)00133-8 rules 10.1016/S0263
  • Aydoğdu, M., 2009. A new shear deformation theory for laminated composite Structures 10.1016/j.compstruct.2008.07.00
  • Felix, D.H., Bambill, D.V.,Rossit, C.A., 2011. A note on buckling and vibration of clamped orthotropic plates under in-plane loads. Struct. Eng. Mech., 39 (1), 115- 123,DOI:10.12989/sem.2011.39. 1.115
  • Aydoğdu, M., Tımarcı, T., 2004. Düzlem-içi destekli dikdörtgen plakların burkulma ve titreşimi, Trakya Univ J Sci, 5(2): 167-177.
  • Aydoğdu, M., Aksencer, T., 2017. Buckling of Cross-ply Composite Plates with Linearly Varying In- plane Loads, 3 January,
  • Kumar, Y., 2017. The Rayleigh– Ritz method for linear dynamic, static and buckling behavior of beams, shells and plates: A literature review, Journal of Vibration and Control, 1-23
  • Noor, A.K., Burton W.S., 1989. Assesment of shear deformation theories composite plates, Appl Mech Rev. 42 (1),DOI:10.1115/1.3152418
  • Noor, A.K., Burton W.S., 1990. Assesment model for multilayered composite plates, Appl Mech Rev., 43 (4): 67-97.DOI: 8223(90)90050-O
  • Mallikarjuna, Kant, T., 1993. A critical review and some results of recently developed refined theories laminated sandwiches, Structures, 312.DOI:10.1016/0263- 8223(93)90230-N and Composite 23 293
  • Altunsaray, E., Bayer, İ., 2004. Buckling laminated quasi-isotropic thin rectangular plates, Steel Compos. Struct., Int. J.,17(3),305-320. DOI: http://dx.doi.org/10.12989/scs.2 014.17.3.305
  • Tsai, S.W., 1988. Composites design, Composites. Think
  • Reddy, J.N, 2004. Mechanics of Laminated Composite Plates and Shells: Theory and Analysis, Second edition, CRC Pres.
  • Ashton, J.E., Whitney, J.M., 1970, Theory of Laminated Plates, Technomic Publication, USA.
  • ANSYS 17 Academic, 2017.

SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI

Year 2017, Volume: 19 Issue: 56, 553 - 568, 01.05.2017

Abstract

Bu çalışmada simetrik katmanlı ince dikdörtgen kompozit plakların Laminasyon Plak Teorisi’nin (KLPT) denklemlerine göre RayleighRitz Yöntemi (R-R) ile gerçekleştirilmiştir. Kenarlarından basit mesnetli, düzlemsel yükleme etkisindeki (Nx) 24 farklı dizilimli kompozit plakın kritik burkulma yükü (N), 12 farklı kenar oranı (a/b ve b/a) için parametrik olarak hesaplanmıştır. Sonuçlar Sonlu Elemanlar Yöntemi (SEY) temelli ANSYS paket yazılımı sonuçlarıyla karşılaştırılmış ve yakın sonuçlar elde edilmiştir. Bu çalışmanın amacı; hazırlanan boyutsuz tabloların kullanımıyla uygun plak tiplerinin bulunması ve kompozit teknelerin yapısal ön tasarımında kullanılacak pratik bilgiler elde edilmesidir. Böylelikle üretim sırasında, malzeme, iş gücü, zaman ve test maliyetlerinden tasarruf edilmesi öngörülmüştür

References

  • Reuben, R.L. 1994. Materials in Marine Technology. Springer- Verlag, London Limited, UK.
  • Shenoi, R.A., Wellicome, J.F. 1993. Composite Materials in Maritime Structures, (Fundamental Cambridge University Pres, NY. Aspects),
  • Shenoi, R.A., Wellicome, J.F. 1993. Composite Materials in Maritime Structures, Volume-II (Practical Considerations), University Pres, NY.
  • Mouritz, A.P., Gellert, E., Burchill, P., Challis K., 2001. Review of Advanced Composite Structures for Naval Ships and Submarines, Composite Structures, Cilt. 53, s..21-41.DOI:10.1016/S0263- 8223(00)00175-6
  • Savcı, M., 1987. Gemi Yapısında Levhalar ve Silindirik Kabuklar, İ.T.Ü. Gemi İnş. ve Deniz Bil. Fak, İstanbul.
  • Lekhnitskii, S.G.1968. Anisotropic Plates, NewYork. Breach, Malzemeler, İ.T.Ü. Sayı:1420,
  • Powell, P.C., 1994. Engineering with fibre-polymer laminates, Chapman & Hall, London, UK.
  • Mallick. P. K., 1997. Composites engineering handbook, Marcel Dekker Inc., NY.
  • ASM Handbook, 2001. Volume 21, Composites, ASM International.
  • Harper, C.A., 2002. Handbook of plastics, composites, McGraw-Hill, NY. and
  • Ambartsumyan, S.A, 1970. Theory of Anisotropic Plates, Technomic Publishing, Co., Wesport Conn.
  • Baharlou, B., Leissa A.W., 1987. Vibration Generally Laminated Composite Plates conditions, Int. J. Mech. Sci. Vol. 29, No. 8, pp. 545-555.DOI: 10.1016/0020-7403(87)90026-9
  • Lakshminarayana, L., Kumar, Krishna Mohana Rao G., 2012. Buckling isotropic quasi- symmetrically laminated rectangular composite plates with an elliptical/circular cutout subjected to linearly varying in-plane loading using FEM, International Journal Of Mechanics, Issue 1, Volume 6.
  • Hu, H., Badir, A., Abatan, A., 2003. Buckling graphite/epoxy composite plate under parabolic variation of axial loads, Int. J. Mech. Sci. 45, 1135– 1147.DOI:10.1016/j.ijmecsci.200 3.08.003 of a
  • Darvizeh, M., Darvizeh, A., Ansari, R., Sharma, C.B., 2004. Buckling analysis of generally laminated composite plates (generalized differential versus Rayleigh–Ritz method), Composite Structures 63, 69– 74.DOI: 8223(03)00133-8 rules 10.1016/S0263
  • Aydoğdu, M., 2009. A new shear deformation theory for laminated composite Structures 10.1016/j.compstruct.2008.07.00
  • Felix, D.H., Bambill, D.V.,Rossit, C.A., 2011. A note on buckling and vibration of clamped orthotropic plates under in-plane loads. Struct. Eng. Mech., 39 (1), 115- 123,DOI:10.12989/sem.2011.39. 1.115
  • Aydoğdu, M., Tımarcı, T., 2004. Düzlem-içi destekli dikdörtgen plakların burkulma ve titreşimi, Trakya Univ J Sci, 5(2): 167-177.
  • Aydoğdu, M., Aksencer, T., 2017. Buckling of Cross-ply Composite Plates with Linearly Varying In- plane Loads, 3 January,
  • Kumar, Y., 2017. The Rayleigh– Ritz method for linear dynamic, static and buckling behavior of beams, shells and plates: A literature review, Journal of Vibration and Control, 1-23
  • Noor, A.K., Burton W.S., 1989. Assesment of shear deformation theories composite plates, Appl Mech Rev. 42 (1),DOI:10.1115/1.3152418
  • Noor, A.K., Burton W.S., 1990. Assesment model for multilayered composite plates, Appl Mech Rev., 43 (4): 67-97.DOI: 8223(90)90050-O
  • Mallikarjuna, Kant, T., 1993. A critical review and some results of recently developed refined theories laminated sandwiches, Structures, 312.DOI:10.1016/0263- 8223(93)90230-N and Composite 23 293
  • Altunsaray, E., Bayer, İ., 2004. Buckling laminated quasi-isotropic thin rectangular plates, Steel Compos. Struct., Int. J.,17(3),305-320. DOI: http://dx.doi.org/10.12989/scs.2 014.17.3.305
  • Tsai, S.W., 1988. Composites design, Composites. Think
  • Reddy, J.N, 2004. Mechanics of Laminated Composite Plates and Shells: Theory and Analysis, Second edition, CRC Pres.
  • Ashton, J.E., Whitney, J.M., 1970, Theory of Laminated Plates, Technomic Publication, USA.
  • ANSYS 17 Academic, 2017.
There are 28 citations in total.

Details

Other ID JA93AJ59UU
Journal Section Research Article
Authors

Erkin Altunsaray This is me

Publication Date May 1, 2017
Published in Issue Year 2017 Volume: 19 Issue: 56

Cite

APA Altunsaray, E. (2017). SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI. Dokuz Eylül Üniversitesi Mühendislik Fakültesi Fen Ve Mühendislik Dergisi, 19(56), 553-568.
AMA Altunsaray E. SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI. DEUFMD. May 2017;19(56):553-568.
Chicago Altunsaray, Erkin. “SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI”. Dokuz Eylül Üniversitesi Mühendislik Fakültesi Fen Ve Mühendislik Dergisi 19, no. 56 (May 2017): 553-68.
EndNote Altunsaray E (May 1, 2017) SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI. Dokuz Eylül Üniversitesi Mühendislik Fakültesi Fen ve Mühendislik Dergisi 19 56 553–568.
IEEE E. Altunsaray, “SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI”, DEUFMD, vol. 19, no. 56, pp. 553–568, 2017.
ISNAD Altunsaray, Erkin. “SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI”. Dokuz Eylül Üniversitesi Mühendislik Fakültesi Fen ve Mühendislik Dergisi 19/56 (May 2017), 553-568.
JAMA Altunsaray E. SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI. DEUFMD. 2017;19:553–568.
MLA Altunsaray, Erkin. “SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI”. Dokuz Eylül Üniversitesi Mühendislik Fakültesi Fen Ve Mühendislik Dergisi, vol. 19, no. 56, 2017, pp. 553-68.
Vancouver Altunsaray E. SİMETRİK KATMANLI İNCE DİKDÖRTGEN KOMPOZİT PLAKLARIN BURKULMASI. DEUFMD. 2017;19(56):553-68.

Dokuz Eylül Üniversitesi, Mühendislik Fakültesi Dekanlığı Tınaztepe Yerleşkesi, Adatepe Mah. Doğuş Cad. No: 207-I / 35390 Buca-İZMİR.