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A parametric study of optimum designs for benchmark stiffened wing panels

  • Published:1993-01 Issue:7-8 Volume:3 Page:619-632
  • ISSN:0961-9526
  • Container-title:Composites Engineering
  • language:en
  • Short-container-title:Composites Engineering

Author:

York C.B.,Williams F.W.,Kennedy D.,Butler R.

Publisher

Elsevier BV

Subject

General Engineering

Reference18 articles.

1. Inclusion of transverse shear deformation in exact buckling and vibration analysis of composite plate assemblies;Anderson,1992

2. General panel sizing computer code and its application to composite structural panels;Anderson;AIAA J,1979

3. PANOPT user manual;Arendsen,1991

4. Buckling of prismatic structures under biaxial loading;Ashour;Comput. Structs,1980

5. PANDA2—program for minimum weight design of stiffened, composite, locally buckled panels;Bushnell;Comput. Structs,1986

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1. Laminate stiffness tailoring for improved buckling performance;Thin-Walled Structures;2021-04

2. Compression and shear buckling performance of finite length plates with bending-twisting coupling;Composite Structures;2020-06

3. Multilevel framework for optimization of lightweight structures;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2012-01-19

4. Buckling Analysis and Minimum-Mass Design Procedures for Composite Wing-Box Structures;Journal of Aircraft;2006-03

5. Buckling of Skew Plates with Continuity or Rotational Edge Restraint;Journal of Aerospace Engineering;2001-07
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