مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Verion

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

video

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

sound

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Persian Version

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

View:

636
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Download:

0
مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Cites:

Information Journal Paper

Title

Postbuckling Analysis of Laminated Composites with Cutout Using Experimental, Numerical, and Finite Strip Methods

Pages

  2067-2077

Abstract

 The optimal design of multilayer substrates containing the cutout under compression is very important to achieve maximum buckling resistance in comparison with structural weight, especially in aerospace structures. In this study, buckling and Post-Buckling behavior of composite laminated plates with orthogonal and symmetrical layup containing the cutout with different diameters has been investigated experimentally, semi-analytically, and numerically. To study the buckling of the composite plate with cutout semi-analytically, a Finite Strip Method is developed. A finite element method was used for numerical analysis. The required material parameters for modeling were obtained from standard tests. The results of the current study show that the size of diameter of cutout does not have considerable effect on elastic rigidity of plate, but the buckling load significantly decreases by increasing cutout diameter. Also, buckling load and elastic rigidity of plate are considerably increased by increasing the number of composite layers. The thickness of plate has more effect on buckling load than the diameter of hole. Studies show that there is a good match between the results of buckling behavior derived from semi-analytical and finite element methods with experimental results.

Cites

  • No record.
  • References

  • No record.
  • Cite

    APA: Copy

    SHOJAEE, T., MOHAMMADI, B., & MADOLIAT, R.. (2019). Postbuckling Analysis of Laminated Composites with Cutout Using Experimental, Numerical, and Finite Strip Methods. MODARES MECHANICAL ENGINEERING, 19(8 ), 2067-2077. SID. https://sid.ir/paper/178205/en

    Vancouver: Copy

    SHOJAEE T., MOHAMMADI B., MADOLIAT R.. Postbuckling Analysis of Laminated Composites with Cutout Using Experimental, Numerical, and Finite Strip Methods. MODARES MECHANICAL ENGINEERING[Internet]. 2019;19(8 ):2067-2077. Available from: https://sid.ir/paper/178205/en

    IEEE: Copy

    T. SHOJAEE, B. MOHAMMADI, and R. MADOLIAT, “Postbuckling Analysis of Laminated Composites with Cutout Using Experimental, Numerical, and Finite Strip Methods,” MODARES MECHANICAL ENGINEERING, vol. 19, no. 8 , pp. 2067–2077, 2019, [Online]. Available: https://sid.ir/paper/178205/en

    Related Journal Papers

    Related Seminar Papers

  • No record.
  • Related Plans

  • No record.
  • Recommended Workshops






    Move to top
    telegram sharing button
    whatsapp sharing button
    linkedin sharing button
    twitter sharing button
    email sharing button
    email sharing button
    email sharing button
    sharethis sharing button