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Data-driven modelling and optimization of stiffeners on undevelopable curved surfaces

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Abstract

Undevelopable stiffened curved shells have been widely used in engineering fields. The shape of the undevelopable curved surface is generally characterized with the non-straight generatrix and variable cross sections, which makes it challenging to automatically model and optimize stiffeners on the undevelopable curved surface. Therefore, the data-driven modelling and optimization framework are proposed for undevelopable stiffened curved shells in this paper. Firstly, a novel mesh deformation method is developed for the data-driven modelling of undevelopable stiffened curved shells based on RBF neural network machine learning method. Its main idea is to firstly define a developable curved shell (background mesh domain) having similar topological characteristics with the undevelopable curved shell (target mesh domain), and then train the mapping relationship between the background mesh domain and the target mesh domain by RBF neural network, and finally the complicated modelling problem of the undevelopable stiffened curved shell can be transformed into a simple modelling problem of developable stiffened curved shell by means of the mapping relationship. Moreover, based on the efficient global optimization (EGO) surrogate method, a data-driven layout optimization method is established for minimizing the structural weight of undevelopable stiffened curved shells. Finally, three representative optimization examples are carried out, including modelling and optimization of stiffeners on hyperbolic parabolic curved surfaces, blade-shaped curved surfaces and S-shaped variable cross-sectional curved surfaces. Optimal results indicate that the structural weight of undevelopable stiffened curved shells decreases significantly after the optimization, indicating the effectiveness of the proposed modelling and optimization framework.

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References

  • Abedinia O, Amjady N (2016) Short-term load forecast of electrical power system by radial basis function neural network and new stochastic search algorithm. Int Trans Electr Energy Syst 26(7):1511–1525

    Google Scholar 

  • Batina JT (1990) Unsteady Euler airfoil solutions using unstructured dynamic meshes. AIAA J 28(8):1381–1388

    Google Scholar 

  • Cheng W, Wang Z, Zhou L et al (2017) Influences of shield ratio on the infrared signature of serpentine nozzle. Aerosp Sci Technol 71:299–311

    Google Scholar 

  • Deaton J, Grandhi R (2010) Thermal-structural analysis of engine exhaust-washed structures. 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, 9236

  • Ding S, Chang X H. A MATLAB-based study on the realization and approximation performance of RBF neural networks. Applied mechanics and materials. Trans Tech Publications, 2013, 325: 1746–1749

  • Du B, Chen LM, Wu W et al (2018) A novel hierarchical thermoplastic composite honeycomb cylindrical structure: fabrication and axial compressive properties. Compos Sci Technol 164:136–145

    Google Scholar 

  • Elsayed K, Lacor C (2014) Robust parameter design optimization using Kriging, RBF and RBFNN with gradient-based and evolutionary optimization techniques. Appl Math Comput 236:325–344

    MathSciNet  MATH  Google Scholar 

  • Hao P, Wang B, Tian K et al (2016) Efficient optimization of cylindrical stiffened shells with reinforced cutouts by curvilinear stiffeners. AIAA J 54(1):1350–1363

    Google Scholar 

  • Hao P, Wang B, Tian K et al (2017) Fast procedure for non-uniform optimum design of stiffened shells under buckling constraint. Struct Multidiscip Optim 55(4):1503–1516

    MathSciNet  Google Scholar 

  • Ji J, Ding XH, Xiong M (2014) Optimal stiffener layout of plate/shell structures by bionic growth method. Comput Struct 135:88–99

    Google Scholar 

  • Jiang S, Sun FF, Fan HL et al (2017) Fabrication and testing of composite orthogrid sandwich cylinder. Compos Sci Technol 142:171–179

    Google Scholar 

  • Jones DR, Schonlau M, Welch WJ (1998) Efficient global optimization of expensive black-box functions. J Glob Optim 13(4):455–492

    MathSciNet  MATH  Google Scholar 

  • Keshtegar B, Hao P (2018a) A hybrid descent mean value for accurate and efficient performance measure approach of reliability-based design optimization. Comput Methods Appl Mech Eng 336:237–259

    MathSciNet  MATH  Google Scholar 

  • Keshtegar B, Hao P (2018b) Enhanced single-loop method for efficient reliability-based design optimization with complex constraints. Struct Multidiscip Optim 57(4):1–17

    MathSciNet  Google Scholar 

  • Keshtegar B, Hao P, Wang Y et al (2017) Optimum design of aircraft panels based on adaptive dynamic harmony search. Thin-Walled Struct 118:37–45

    Google Scholar 

  • Kulkarni MMS, Aliasgher L (2014) Analysis of tensile fabric structure using thin concrete doubly curved shell. Int J Res Advent Technol 2(3):156–165

    Google Scholar 

  • Lee CC, Boedicker C (1985) Subsonic diffuser design and performance for advanced fighter aircraft. Aircraft Design Systems and Operations Meeting 3073

  • Li BT, Hong J, Liu Z (2014) Stiffness design of machine tool structures by a biologically inspired topology optimization method. Int J Mach Tools Manuf 84:33–44

    Google Scholar 

  • Li M, Sun FF, Lai CL et al (2018) Fabrication and testing of composite hierarchical isogrid stiffened cylinder. Compos Sci Technol 157:152–159

    Google Scholar 

  • Li YF, Wang YT, Ma R et al (2019a) Improved reliability-based design optimization of non-uniformly stiffened spherical dome. Struct Multidiscip Optim 60(1):375–392

    Google Scholar 

  • Li L, Wan H, Gao W et al (2019b) Reliability based multidisciplinary design optimization of cooling turbine blade considering uncertainty data statistics. Struct Multidiscip Optim 59(2):659–673

    Google Scholar 

  • Li L, Yuan T, Li Y et al (2019c) Multidisciplinary design optimization based on parameterized free-form deformation for single turbine. AIAA J 57(5):2075–2087

    Google Scholar 

  • Liu Y, Shimoda M (2015) Non-parametric shape optimization method for natural vibration design of stiffened shells. Comput Struct 146:20–31

    Google Scholar 

  • Liu X, Qin N, Xia H (2006) Fast dynamic grid deformation based on Delaunay graph mapping. J Comput Phys 211(2):405–423

    MATH  Google Scholar 

  • Martin-Burgos MJ, González-Juárez D, Andrés-Pérez E (2017) A novel surface mesh deformation method for handling wing-fuselage intersections. Chin J Aeronaut 30(1):264–273

    Google Scholar 

  • Meng Z, Hao P, Li G et al (2015) Non-probabilistic reliability-based design optimization of stiffened shells under buckling constraint. Thin-Walled Struct 94:325–333

    Google Scholar 

  • Mulani SB, Slemp WCH, Kapania RK (2013) EBF3PanelOpt: an optimization framework for curvilinear blade-stiffened panels. Thin-Walled Struct 63:13–26

    Google Scholar 

  • Ning X, Pellegrino S (2015) Imperfection-insensitive axially loaded thin cylindrical shells. Int J Solids Struct 62:39–51

    Google Scholar 

  • Rahimi GH, Zandi M, Rasouli SF (2013) Analysis of the effect of stiffener profile on buckling strength in composite isogrid stiffened shell under axial loading. Aerosp Sci Technol 24(1):198–203

    Google Scholar 

  • Rendall TCS, Allen CB (2009) Efficient mesh motion using radial basis functions with data reduction algorithms. J Comput Phys 228(17):6231–6249

    MATH  Google Scholar 

  • Shi P, Kapania RK, Dong CY (2015) Free vibration of curvilinearly stiffened shallow shells. J Vib Acoust 137(3):031006

    Google Scholar 

  • Shi P, Kapania R K, Dong C (2050) Free vibration analysis of curvilinearly stiffened cylindrical shells. 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2015

  • Stanford B, Beran P, Bhatia M (2014) Aeroelastic topology optimization of blade-stiffened panels. J Aircr 51(3):938–944

    Google Scholar 

  • Sun X, Wang Z, Zhou L et al (2016) Influences of design parameters on a double serpentine convergent nozzle. J Eng Gas Turbines Power 138(7):072301

    Google Scholar 

  • Tian K, Wang B, Zhang K et al (2018) Tailoring the optimal load-carrying efficiency of hierarchical stiffened shells by competitive sampling. Thin-Walled Struct 133:216–225

    Google Scholar 

  • Tomás A, Tovar JP (2012) The influence of initial geometric imperfections on the buckling load of single and double curvature concrete shells. Comput Struct 96:34–45

    Google Scholar 

  • Tornabene F, Fantuzzi N, Bacciocchi M et al (2016) Effect of agglomeration on the natural frequencies of functionally graded carbon nanotube-reinforced laminated composite doubly-curved shells. Compos Part B 89:187–218

    Google Scholar 

  • Wagner HNR, Hühne C, Niemann S (2018) Robust knockdown factors for the design of spherical shells under external pressure: development and validation. Int J Mech Sci 141:58–77

    Google Scholar 

  • Wagner HNR, Hühne C, Zhang J et al (2019) Geometric imperfection and lower-bound analysis of spherical shells under external pressure. Thin-Walled Struct 143:106195

    Google Scholar 

  • Wang D, Abdalla MM (2015) Global and local buckling analysis of grid-stiffened composite panels. Compos Struct 119:767–776

    Google Scholar 

  • Wang D, Zhang WH (2012) A bispace parameterization method for shape optimization of thin-walled curved shell structures with openings. Int J Numer Methods Eng 90(13):1598–1617

    MathSciNet  MATH  Google Scholar 

  • Wang B, Hao P, Li G et al (2014a) Two-stage size-layout optimization of axially compressed stiffened panels. Struct Multidiscip Optim 50(2):313–327

    Google Scholar 

  • Wang B, Hao P, Li G et al (2014b) Generatrix shape optimization of stiffened shells for low imperfection sensitivity. SCIENCE CHINA Technol Sci 57(10):2012–2019

    Google Scholar 

  • Wang B, Tian K, Hao P et al (2016a) Numerical-based smeared stiffener method for global buckling analysis of grid-stiffened composite cylindrical shells. Compos Struct 152:807–815

    Google Scholar 

  • Wang CF, Xu YM, Du JW (2016b) Study on the thermal buckling and post-buckling of metallic sub-stiffening structure and its optimization. Mater Struct 49(11):4867–4879

    Google Scholar 

  • Wang G, Chen X, Liu ZK (2018) Mesh deformation on 3D complex configurations using multistep radial basis functions interpolation. Chin J Aeronaut 31(4):660–671

    Google Scholar 

  • Wang D, Abdalla MM, Wang ZP et al (2019) Streamline stiffener path optimization (SSPO) for embedded stiffener layout design of non-uniform curved grid-stiffened composite (NCGC) structures. Comput Methods Appl Mech Eng 344:1021–1050

    MathSciNet  MATH  Google Scholar 

  • Wu H, Lai C, Sun FF et al (2018) Carbon fiber reinforced hierarchical orthogrid stiffened cylinder: fabrication and testing. Acta Astronautica 145:268–274

    Google Scholar 

  • Yun Z, Quan Z, Caixin S et al (2008) RBF neural network and ANFIS-based short-term load forecasting approach in real-time price environment. IEEE Trans Power Syst 23(3):853–858

    Google Scholar 

  • Zhang WH, Wang D, Yang JG (2010) A parametric mapping method for curve shape optimization on 3D panel structures. Int J Numer Methods Eng 84(4):485–504

    MATH  Google Scholar 

  • Zhao W, Kapania RK (2016) Vibration analysis of curvilinearly stiffened composite panel subjected to in-plane loads. AIAA J 55(3):981–997

    Google Scholar 

  • Zhao YN, Chen MJ, Yang F et al (2017) Optimal design of hierarchical grid-stiffened cylindrical shell structures based on linear buckling and nonlinear collapse analyses. Thin-Walled Struct 119:315–323

    Google Scholar 

Download references

Acknowledgements

Special thanks to Mr. Ke Zhang and Mr. Yan Zhou from Dalian University of Technology for their help in EGO method and FE modelling.

Replication of results

The codes for the RBFNN approach used in the mesh deformation method and the EGO method are written in MATLAB, which are named as “RBFNN” and “EGO” in the supplemental material. In addition, the control point sets used in the mesh deformation method are attached in the supplemental material, including the undevelopable hyperbolic parabolic curved surface, the developable flat plate, the undevelopable blade with non-straight generatrix, the developable blade with straight generatrix, the undevelopable S-shaped variable cross-sectional curved surface and the developable cylindrical shell, which are all provided in EXCEL format.

Funding

This work was supported by National Natural Science Foundation of China [no. 11902065 and no. 11825202], China Postdoctoral Science Foundation [no. 2019M651107] and LiaoNing Revitalization Talents Program [no. XLYC1802020].

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Appendices

Appendix 1. RBFNN algorithm

The structure of RBFNN is displayed in Fig. 30. When the input is Xi, the output of the jth node in the hidden layer can be expressed as

$$ G\left({X}_i,{C}_j,{\sigma}_j\right)=\exp \left(-\left\Vert {X}_i-{C}_j\right\Vert /2{\sigma}_j^2\right) $$
(11)

where Cj = (cj1, cj2,…, cjn)T and σj are the center and width of the Gaussian function of the jth node in the hidden layer, respectively.

For an input Xi, the expected output Yi is

$$ {Y}_i=\sum \limits_{j=1}^MG\left({X}_1,{C}_j,{\sigma}_j\right){\omega}_j+{e}_i $$
(12)

where ωj represents the weight between the jth neuron of the hidden layer and output neuron. M is the neuron number in the hidden layer. ei represents the fitting error.

Fig. 30
figure 30

Schematic diagrams of RBF neural network

Appendix 2. EGO algorithm

The flow chart of EGO method is displayed in Fig. 31. Firstly, sampling points are generated in the design space by Latin hypercube sampling (LHS) method. Secondly, a kriging surrogate model is constructed based on sampling results. Thirdly, the expectation of improvement EI of the kriging surrogate model at each sampling point x is evaluated,

$$ EI(x)=\left({y}_{\mathrm{min}}-\hat{y}\left(\left.x\right)\right)\Phi \left(\frac{y_{\mathrm{min}}-\hat{y}(x)}{s(x)}\right)+s(x)\phi \left(\frac{y_{\mathrm{min}}-\hat{y}(x)}{s(x)}\right)\right) $$
(13)

where ymin represents the optimal result of each update, \( \hat{y}(x) \) represents the prediction mean value of kriging surrogate model, and s(x) represents the prediction standard deviation of kriging surrogate model. Φ(·) and ϕ(·) are the cumulative density function and probability density function of a normal distribution, respectively. In this presented work, the kriging model considered in the EGO algorithm is based on the Gaussian kernel.

Fourthly, MIGA is employed to search for the optimal result aiming at maximizing the EI. Finally, the stop criterion is estimated, which includes three conditions: (1) The maximum EI value is smaller than the tolerance (1e-4 in this paper); (2) the distance between the current iteration point and the former iteration point is smaller than the tolerance (1e-4 in this paper); (3) the iteration number reaches the maximum value. Once one of these three conditions are satisfied, the EGO is stopped. If the stop criterion is not satisfied, the new sampling point can be chosen by maximizing the EI and added into the original kriging surrogate model. This process repeats until the stop criterion is satisfied.

Fig. 31
figure 31

Flow chart of EGO method

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Tian, K., Li, H., Huang, L. et al. Data-driven modelling and optimization of stiffeners on undevelopable curved surfaces. Struct Multidisc Optim 62, 3249–3269 (2020). https://doi.org/10.1007/s00158-020-02675-4

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