Damage Tolerance Predictions for Stiffened Composite Panels—Part II: Application of a Failure Criteria

1996 ◽  
Vol 18 (2) ◽  
pp. 102 ◽  
Author(s):  
WS Johnson ◽  
JE Masters ◽  
DW Wilson ◽  
DL Graesser ◽  
ME Tuttle
2001 ◽  
Vol 35 (20) ◽  
pp. 1815-1843 ◽  
Author(s):  
Puhui Chen ◽  
Zhen Shen ◽  
Junyang Wang

2006 ◽  
Vol 25 (13) ◽  
pp. 1341-1351 ◽  
Author(s):  
Faruk Elaldi ◽  
Sezgin Alecakir

2011 ◽  
Vol 314-316 ◽  
pp. 963-967
Author(s):  
Li Liang ◽  
Pu Rong Jia ◽  
Gui Qiong Jiao

In this paper experimental and FEA methods were used to study the damage propagation and failure properties of stiffened composite panels with discrete-source damage. The influence of discrete-source damage on residual strength of the composite panel was also investigated. The research results indicated that notched composite panel was suitable to simulate the damage property of stiffened composite panel with discrete-source damage. It has showed that there is high strain concentration at the notch end. And break-through of the stringer can make the load path changed. Based on different failure criteria, FEA method with progressive failure procedure was used to simulate the damage progression and failure procedure of the notched stiffened composite panel effectively. The analytical result was in good correspondence with the experimental data.


Author(s):  
Jerry G. Williams ◽  
Melvin S. Anderson ◽  
Marvin D. Rhodes ◽  
James H. Starnes ◽  
W. Jefferson Stroud

1996 ◽  
Vol 18 (1) ◽  
pp. 47 ◽  
Author(s):  
WS Johnson ◽  
JE Masters ◽  
DW Wilson ◽  
DL Graesser ◽  
ME Tuttle

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