THREE POINT BENDING TEST ON CFRP BLADE STIFFENED PANEL
<p align="justify"> in this research, a Carbon Fiber Reinforced Polymer (CFRP) blade stiffened panel was three point bending test. The previous research about three point bending numerical analysis on CFRP blade stiffened panel by Jacky (2017) used as an answer in building concepts...
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id-itb.:277412018-09-26T16:31:56ZTHREE POINT BENDING TEST ON CFRP BLADE STIFFENED PANEL (NIM: 23616011), HARIYANTO Indonesia Theses INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/27741 <p align="justify"> in this research, a Carbon Fiber Reinforced Polymer (CFRP) blade stiffened panel was three point bending test. The previous research about three point bending numerical analysis on CFRP blade stiffened panel by Jacky (2017) used as an answer in building concepts and also comparing the results of tests with numerical models that have been done before. The results obtained are quite different from numerical models (Jacky ,2017) with test result, the <br /> <br /> graphs and failure mode. In terms of the graph of force Vs elongation, the test result of a more upward trend than numerical (Jacky, 2017). <br /> <br /> In terms of modus failure, results differ fundamentally. Numerical results (Jacky, 2017) indicate fiber breakage failure but the test <br /> <br /> results is delamination. <br /> <br /> The average maximum load that can be achieved in testing is 6 tonsor equivalent to 58.84 kN. This level of yield is still lower than the numerical results (Jacky,2017) reaching at 69.8 kN. <p align="justify"> text |
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<p align="justify"> in this research, a Carbon Fiber Reinforced Polymer (CFRP) blade stiffened panel was three point bending test. The previous research about three point bending numerical analysis on CFRP blade stiffened panel by Jacky (2017) used as an answer in building concepts and also comparing the results of tests with numerical models that have been done before. The results obtained are quite different from numerical models (Jacky ,2017) with test result, the <br />
<br />
graphs and failure mode. In terms of the graph of force Vs elongation, the test result of a more upward trend than numerical (Jacky, 2017). <br />
<br />
In terms of modus failure, results differ fundamentally. Numerical results (Jacky, 2017) indicate fiber breakage failure but the test <br />
<br />
results is delamination. <br />
<br />
The average maximum load that can be achieved in testing is 6 tonsor equivalent to 58.84 kN. This level of yield is still lower than the numerical results (Jacky,2017) reaching at 69.8 kN. <p align="justify"> |
| format |
Theses |
| author |
(NIM: 23616011), HARIYANTO |
| spellingShingle |
(NIM: 23616011), HARIYANTO THREE POINT BENDING TEST ON CFRP BLADE STIFFENED PANEL |
| author_facet |
(NIM: 23616011), HARIYANTO |
| author_sort |
(NIM: 23616011), HARIYANTO |
| title |
THREE POINT BENDING TEST ON CFRP BLADE STIFFENED PANEL |
| title_short |
THREE POINT BENDING TEST ON CFRP BLADE STIFFENED PANEL |
| title_full |
THREE POINT BENDING TEST ON CFRP BLADE STIFFENED PANEL |
| title_fullStr |
THREE POINT BENDING TEST ON CFRP BLADE STIFFENED PANEL |
| title_full_unstemmed |
THREE POINT BENDING TEST ON CFRP BLADE STIFFENED PANEL |
| title_sort |
three point bending test on cfrp blade stiffened panel |
| url |
https://digilib.itb.ac.id/gdl/view/27741 |
| _version_ |
1821934472356954112 |