In this paper, CFRP specimens were manufactured with the configuration of mode Ⅰ,Ⅱ to which variously different fiber laminate angles were applied. The reliability on the tensile characteristics at the adhesive interface according to the fiber laminate angle of the structure bonded by using an adhesive is confirmed through the analysis and experiment carried out in advance. Although there were a lot of difficulties in the design and assessment since the anisotropy of fiber reinforced composite material has the highest strength and rigidity characteristics in the direction of fiber, it is possible to reduce the time and cost incurred by securing the preceding data through the analytic method. It is possible to observe that the displacements of detachment at the adhesive interface differ from each other in both the experiment and analysis results. By applying it to the load conditions of modes Ⅰ and Ⅱ, the static and fatigue experiments were carried out respectively. And the analysis study was conducted in case of static experiment. The feed speed of 3mm/min was progressed at the static test. And the load of 1 kN with 10 Hz was carried at the fatigue test. Through this kind of experiment, the laminar angle and fracture property at the bonding separation of adhesive interface were understood. Also, the reliability of experimental value could be obtained and the direction and value of stress contour could be understood through the static analysis. And it is thought that the result values of fatigue experiment could be utilized to the data for the structural safety at the structure applied with fatigue load. The study result of this paper is seen to contribute to the structural safety through design parameters of CFRP structure applied with laminate angle among composite materials.