Buckling Analysis of Discretely Stiffened Composite Curved Panels under Compression and Shear

X. X. Tong; B. Geier; K. Rohwer

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Article Navigation > Applied Mathematics and Mechanics > 1986 > 7(4): 295-305

X. X. Tong, B. Geier, K. Rohwer. Buckling Analysis of Discretely Stiffened Composite Curved Panels under Compression and Shear[J]. Applied Mathematics and Mechanics, 1986, 7(4): 295-305.

Citation:

X. X. Tong, B. Geier, K. Rohwer. Buckling Analysis of Discretely Stiffened Composite Curved Panels under Compression and Shear[J]. Applied Mathematics and Mechanics, 1986, 7(4): 295-305.

Citation:

X. X. Tong, B. Geier, K. Rohwer. Buckling Analysis of Discretely Stiffened Composite Curved Panels under Compression and Shear[J]. Applied Mathematics and Mechanics, 1986, 7(4): 295-305.

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Buckling Analysis of Discretely Stiffened Composite Curved Panels under Compression and Shear

1.
Institute for Structural Mechanics of CAE, Beijing;
2.
Institute for Structural Mechanics of DFVLR, West Germany

Received Date: 1985-05-09
Publish Date: 1986-04-15

Abstract

Abstract

An analytical method for the buckling discretely thin-wall stiffened composite curved panels under compression and shear is presented by use of finite strip-element method.In the report a simplified scheme for complex displacement functions is developed.It enables that computation to be performed in real number algebra easily.And a simple and easy way to satisify the boundary conditions is introduced.Numerical results are given and are in good agreement with available data.

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References(7)

References

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