In the spoilers came up with the design principles of aerodynamics. In this study, the organizing committee is in doubt. Factors that affect the pressure of the spoiler, depending on the degree. Or the size of the spoiler. It depends if it is increased or decreased to increase the pressure to have this type of equipment. We have chosen the model of aircraft to be tested. The size of the length and angle versions NACA6412 NACA2412 and NACA0015 degrees at 0:20 and 0:25 is 0.15 meters, so as to make it possible to simulate a wind tunnel. In order to test The results came out, it was. The size of the increase is a result of the pressure of the spoiler on the increase. As a result, the degree to which different forms of spoiler.
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