Nonlinear Buckling and Postbuckling Analysis of Tow-Steered Composite Cylinders with Cutouts

被引:4
作者
Groh, Rainer M. J. [1 ]
Wu, K. C. [2 ]
机构
[1] Univ Bristol, Dept Aerosp Engn, Bristol BS8 1TR, England
[2] NASA Langley Res Ctr, Hampton, VA 23681 USA
关键词
CYLINDRICAL-SHELLS; PANELS; OPTIMIZATION; BEHAVIOR; DESIGN; VIBRATION;
D O I
10.2514/1.J061755
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The buckling and postbuckling behavior of two composite tow-steered shells with cutouts of different sizes is assessed using nonlinear finite element analysis and compared to experimental measurements. The cylindrical shells are manufactured using an automated fiber placement system, where the shells' fiber orientation angles vary continuously around the shell circumference from & PLUSMN;10 deg on the crown and keel to & PLUSMN;45 deg on the sides. One shell features thickness variations due to tow overlaps that result from application of all 24 tows during each pass of the fiber placement system. The second shell uses the system's tow drop/add capability to achieve a more uniform wall thickness without overlaps. Unreinforced cutouts of two different sizes-the first smaller cutout representing a passenger door on a commercial aircraft and the second larger cutout a cargo door-were machined into each of the two cylinders resulting in a total of four test cases. These cylinders were tested in axial compression and buckled elastically in previous work and are now analyzed using nonlinear finite element models to compare bifurcation buckling loads as well as the load-displacement response in the prebuckling and postbuckling regimes. For all four shells analyzed, the prebuckling stiffness, buckling load, and deformation mode sequence throughout the loading-unloading cycle is accurately reproduced by the models. In particular, the shells first buckle locally around the cutouts in a stable (supercritical) manner with only a slight decrease in axial stiffness, which occurs due to the favorable load redistribution facilitated by tow steering. The shells then buckle globally in an unstable (subcritical) manner with diamond-shaped buckles forming to the left and right (circumferential direction) of the cutouts. The buckling load of all shells with cutouts is at least 82% of the buckling load of the pristine shells without cutouts. Overall, the ability to sustain local buckling phenomena, and the relatively small reductions in global buckling load compared to pristine shells without cutouts, demonstrates the great potential of using tow steering to mitigate the adverse effects of cutouts in axially compressed shell structures.
引用
收藏
页码:5533 / 5546
页数:14
相关论文
共 59 条
  • [1] Optimal Design of Tow-Placed Fuselage Panels for Maximum Strength with Buckling Considerations
    Alhajahmad, Ahmad
    Abdalla, Mostafa M.
    Gurdal, Zafer
    [J]. JOURNAL OF AIRCRAFT, 2010, 47 (03): : 775 - 782
  • [2] Design, modeling, optimization, manufacturing and testing of variable-angle filament-wound cylinders
    Almeida, Jose Humberto S., Jr.
    St-Pierre, Luc
    Wang, Zhihua
    Ribeiro, Marcelo L.
    Tita, Volnei
    Amico, Sandro C.
    Castro, Saullo G. P.
    [J]. COMPOSITES PART B-ENGINEERING, 2021, 225
  • [3] Improving the open-hole tension characteristics with variable-axial composite laminates: Optimization, progressive damage modeling and experimental observations
    Almeida, Jose Humberto S., Jr.
    Bittrich, Lars
    Spickenheuer, Axel
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2020, 185
  • [4] [Anonymous], 2018, 2018 STAND US MAN
  • [5] Optimization of a composite cylinder under bending by tailoring stiffness properties in circumferential direction
    Blom, Adriana W.
    Stickler, Patrick B.
    Gurdal, Zafer
    [J]. COMPOSITES PART B-ENGINEERING, 2010, 41 (02) : 157 - 165
  • [6] Bending of Composite Cylindrical Shells with Circular Cutouts: Buckling and Failure Analysis
    Celebi, Mansur
    Gurdal, Zafer
    Tatting, Brian
    Blom-Schieber, Agnes
    Rassaian, Mostafa
    Wanthal, Steven
    Turkmen, Halit Suleyman
    [J]. JOURNAL OF AIRCRAFT, 2019, 56 (04): : 1551 - 1564
  • [7] Buckling analysis of stiffened variable angle tow panels
    Coburn, Broderick H.
    Wu, Zhangming
    Weaver, Paul M.
    [J]. COMPOSITE STRUCTURES, 2014, 111 : 259 - 270
  • [8] Three-dimensional effects influencing failure in bend-free, variable stiffness composite pressure vessels
    Daghighi, Shahrzad
    Weaver, Paul M.
    [J]. COMPOSITE STRUCTURES, 2021, 262
  • [9] Bend -free design of super ellipsoids of revolution composite pressure vessels
    Daghighi, Shahrzad
    Zucco, Giovanni
    Rouhi, Mohammad
    Weaver, Paul M.
    [J]. COMPOSITE STRUCTURES, 2020, 245
  • [10] Groh, 2015, AIAA PAPER 2015 0452, P0452, DOI DOI 10.2514/6.2015-0452