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Nonlinear Out-of-Plane Mechanical Behaviours of Rectangular Woven Composite Flexible Skin Under Uniform Normal Pressure

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Abstract

This paper seeks to investigate nonlinear out-of-plane mechanical behaviours of woven composite flexible skin (WCFS) through experimental and theoretical methods. Firstly, quasi-static experiments are carried out on rectangular WCFSs with different aspect ratios under uniform normal pressure to measure out-of-plane deformation and failure loads. Afterwards, a new three-parameter geometric model is presented to describe 3D geometry of pressurized WCFS, and thus, a nonlinear mechanical model is deduced for depicting the relationship between pressure and out-of-plane displacement. The application of the aforementioned models for experimental results shows that the new models have adequately and logically depicted deformation geometry and nonlinear mechanical characteristics.

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We confirm that the data supporting the research are available within the paper.

Abbreviations

\(a\) :

Half-length of WCFS

\(b\) :

Half-width of WCFS

\(k_{1m}\) :

Slope along the X-axis for plane \(\pi_{1m}\)

\(k_{2n}\) :

Slope along the Y-axis for plane \(\pi_{2n}\)

\(l\) :

Length of thread

\(l_{1}\) :

Length of thread AB

\(l_{2}\) :

Length of thread AC

\(l_{1m}\) :

Length of the mth warp thread

\(l_{2n}\) :

Length of the nth fill thread

\(n_{1}\) :

Number of warp threads on a quarter of WCFS

\(n_{2}\) :

Number of fill threads on a quarter of WCFS

\(N\) :

Tensile load

\(N_{1m}\) :

Tensile load on the mth warp thread

\(N_{2n}\) :

Tensile load on the nth fill thread

\(p\), \(q\), \(\delta\) :

Undetermined parameters

P :

Uniform out-of-plane pressure

R :

Aspect ratio

U :

Strain energy of WCFS

W :

Potential energy generated by out-of-plane pressure

\(\alpha_{1m}\) :

Angle between coordinate plane XOY and the mth warp thread

\(\alpha_{2n}\) :

Angle between coordinate plane XOY and the nth fill thread

\(\beta_{1m}\) :

Angle between coordinate plane YOZ and the mth warp thread

\(\beta_{2n}\) :

Angle between coordinate plane YOZ and the nth fill thread

\(\gamma_{mn}\) :

Shear strain

\(\varphi_{mn}\) :

Angle between the mth warp thread and the nth fill thread

\(\tau_{mn}\) :

Shear stress

\(\varepsilon_{1m}\) :

Tensile strain for the mth warp thread

\(\varepsilon_{2n}\) :

Tensile strain for the nth fill thread

\(\rho_{1}\) :

Fabric density in the warp direction

\(\rho_{2}\) :

Fabric density in the fill direction

\(\mu_{1}\), \(\mu_{2}\), \(\mu_{3}\) :

Material constants

\(\nu_{1}\), \(\nu_{2}\), \(\nu_{3}\) :

Material constants

\({\varDelta}\) :

Centre-point Z-axis displacement of WCFS

\(\Delta l_{1}\) :

Distance between two adjacent intersection points on thread AB

\(\Delta l_{2}\) :

Distance between two adjacent intersection points on thread AC

\(\pi_{1m}\) :

Plane on which the mth warp thread lies

\(\pi_{2n}\) :

Plane on which the nth fill thread lies

Π :

Total potential energy

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Acknowledgements

We appreciate Mr. Dong Li and Mr. Hao-Ming Zhang for providing us with help in the test.

Funding

This project was supported by the National Natural Science Foundation of China (Grant No. 51875021) and China Postdoctoral Science Foundation (Grant No. 2022M720348).

Author information

Authors and Affiliations

Authors

Contributions

DC contributed to investigation, test, data curation, formal analysis, validation, and writing—original draft. J-JX was involved in supervision, conceptualization, methodology, writing—review and editing, and funding acquisition.

Corresponding author

Correspondence to Jun-Jiang Xiong.

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Written informed consent was obtained from individual participants.

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Appendices

Appendix A: Feature Point Coordinates of Planes \(\pi_{1m}\) and \(\pi_{2n}\)

From Fig. 4b, the X-, Y-, and Z-coordinates of points 1 and 2 are, respectively,

$$ x_{1m} = \frac{m - 1}{{n_{1} - 1}}a $$
(A1)
$$ y_{1m} = 0 $$
(A2)
$$ z_{1m} = 0 $$
(A3)

and

$$ x_{2m} = \frac{m - 1}{{n_{1} - 1}}a $$
(A4)
$$ y_{2m} = b $$
(A5)
$$ z_{2m} = 0 $$
(A6)

With the aid of Eq. (9), the X-, Y-, and Z-coordinates of point 3, respectively, satisfy

$$ \int_{0}^{{x_{3m} }} {\sqrt {1 + \left[ {\delta \left( {\ln p} \right)\left( {1 - q^{b} } \right)p^{x} } \right]^{2} } } {\text{d}} x = \left( {m - 1} \right)\Delta l_{2} $$
(A7)
$$ y_{3m} = b $$
(A8)
$$ z_{3m} = \delta \left( {1 - p^{{x_{3m} }} } \right)\left( {1 - q^{b} } \right) $$
(A9)

Likewise, from Fig. 4c, the X-, Y-, and Z-coordinates of points 4 and 5 are, respectively,

$$ x_{4n} = 0 $$
(A10)
$$ y_{4n} = \frac{n - 1}{{n_{2} - 1}}b $$
(A11)
$$ z_{4n} = 0 $$
(A12)

and

$$ x_{5n} = a $$
(A13)
$$ y_{5n} = \frac{n - 1}{{n_{2} - 1}}b $$
(A14)
$$ z_{5n} = 0 $$
(A15)

From Eq. (8), one has

$$ x_{6n} = a $$
(A16)
$$ \int_{0}^{{y_{6n} }} {\sqrt {1 + \left[ {\delta \left( {\ln q} \right)\left( {1 - p^{a} } \right)q^{y} } \right]^{2} } } {\text{d}} y = \left( {n - 1} \right)\Delta l_{1} $$
(A17)
$$ z_{6n} = \delta \left( {1 - p^{a} } \right)\left( {1 - q^{{y_{6n} }} } \right) $$
(A18)

Appendix B: Coordinates of Intersection Points

On the basis of Eqs. (16) and (17), one has

$$ \delta \left( {1 - q^{y} } \right)\left[ {1 - p^{{\frac{{k_{2n} }}{{k_{1m} }}\left( {y - \frac{n - 1}{{n_{2} - 1}}b} \right) + \frac{m - 1}{{n_{1} - 1}}a}} } \right] = k_{2n} \left( {y - \frac{n - 1}{{n_{2} - 1}}b} \right) $$
(B1)

Letting

$$ F\left( y \right) = \delta \left( {1 - q^{y} } \right)\left[ {1 - p^{{\frac{{k_{2n} }}{{k_{1m} }}\left( {y - \frac{n - 1}{{n_{2} - 1}}b} \right) + \frac{m - 1}{{n_{1} - 1}}a}} } \right] - k_{2n} \left( {y - \frac{n - 1}{{n_{2} - 1}}b} \right) $$
(B2)

Equation (B1) turns into

$$ F\left( y \right) = 0 $$
(B3)

It is clear that coordinate \(y_{m,n}\) of the intersection point could be solved by combining Eqs. (B2) and (B3).

Subsequently, coordinates \(z_{m,n}\) and \(x_{m,n}\) of the intersection point are deduced as

$$ z_{m,n} = k_{2n} \left( {y_{m,n} - \frac{n - 1}{{n_{2} - 1}}b} \right) $$
(B4)
$$ x_{m,n} = \frac{{z_{m,n} }}{{k_{1m} }} + \frac{m - 1}{{n_{1} - 1}}a $$
(B5)

Appendix C: Slopes of Threads

In light of Eqs. (25) and (26), the thread slopes at boundary line OB are obtained as

$$ \left( {\frac{\partial z}{{\partial x}}} \right)_{1m} = k_{1m} \, \left( {x = \frac{m - 1}{{n_{1} - 1}}a,y = 0,z = 0} \right) $$
(C1)
$$ \left( {\frac{\partial z}{{\partial y}}} \right)_{1m} = - \delta \left( {\ln q} \right)\left[ {1 - p^{{\frac{m - 1}{{n_{1} - 1}}a}} } \right] \, \left( {x = \frac{m - 1}{{n_{1} - 1}}a,y = 0,z = 0} \right) $$
(C2)

Likewise, the thread slopes at boundary line OC can be solved according to Eqs. (28) and (29), namely

$$ \left( {\frac{\partial z}{{\partial x}}} \right)_{2n} = - \delta \left( {\ln p} \right)\left[ {1 - q^{{\frac{n - 1}{{n_{2} - 1}}b}} } \right] \, \left( {x = 0,y = \frac{n - 1}{{n_{2} - 1}}b,z = 0} \right) $$
(C3)
$$ \left( {\frac{\partial z}{{\partial y}}} \right)_{2n} = k_{2n} \, \left( {x = 0,y = \frac{n - 1}{{n_{2} - 1}}b,z = 0} \right) $$
(C4)

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Chen, D., Xiong, JJ. Nonlinear Out-of-Plane Mechanical Behaviours of Rectangular Woven Composite Flexible Skin Under Uniform Normal Pressure. Acta Mech. Solida Sin. 36, 672–684 (2023). https://doi.org/10.1007/s10338-023-00407-x

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