According to the pilot, he maneuvered the airplane into a slip configuration while on final approach in an effort to compensate for a crosswind. He landed on runway 25 using a wheel-landing technique, where the main landing gear touches down first and the tail gear follows during the landing roll. During the roll out, as the airplane slowed, a gust of wind struck its right side. The airplane began to veer to the right and the pilot attempted to regain directional control with full left rudder and opposing aileron. The airplane continued to veer to the right and flipped over, coming to rest inverted. As a result of the accident sequence, the airplane incurred damage to the left wing, fuselage, vertical stabilizer, and rudder. The pilot reported that there were no preimpact mechanical anomalies with the airplane. The wind reported at the airport about the time of the accident was from 310 degrees at 14 knots, gusting to 19 knots.