Application of Computer in Testing Technology of Interface Strength of Aircraft Composite Materials

Application of computer in testing technology of interface strength of aircraft composite materials is discussed in this study. Due to the particularity of the loading method, the dynamic evaluation method makes the test result closer to the actual use result and has practical guiding significance, but each dynamic evaluation method still has its limitations. To overcome the shortcomings of the traditional model, this paper proposes the computer integrated model for the comprehensive analysis. The system is implemented and tested on the scenario if aircraft composite materials. The results reflected that the framework can well assist the analysis of the data.