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History of NASA Icing Research Tunnel

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History of NASA Icing Research Tunnel ( history-nasa-icing-research-tunnel )

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A different model was developed for Ohio State’s 7 x 10-foot tunnel. Model makers used machinable plastic (Ren Shape) to construct a 2-D airfoil with a 4.75-foot chord and 7-foot span. It was intended to replicate the two-section geometry of the Twin Otter and included an elevator that could be set at various angles. Ratvasky next turned to selecting accurate ice shapes for testing. He wanted to begin in the IRT, but the NASA facility was so heavily scheduled that he decided to use Ohio State’s tunnel for the initial aero-performance tests. One ice shape to be attached to the model had been developed from one of NASA’s icing flights in 1984. Another was derived from LEWICE predictions. The two shapes were machined from Ren Shape, then sanded smooth and painted. Initial tests at Ohio State began in September 1994. Data on the model was first taken without ice shapes in order to establish a baseline. The two ice shapes were then attached to the airfoil, and measurements were made at various airspeeds, elevator angles, and angles of attack. Just as the Ohio State tests concluded, the American Eagle accident at Roselawn occurred, focusing attention on the more urgent problem of large droplet icing. As noted earlier, Ratvasky joined the NTSB team that investigated the ATR 72 accident. Ratvasky was not able to turn his attention to the Tailplane Icing Program until the fall of 1995. The next phase of the program involved flight tests to establish a baseline against which to measure the effects of tailplane contamination. In September and October, the Twin Otter made seventeen flights. While pilots Ranaudo and Dennis O’Donoghue confirmed the operation of the airplane’s hydraulic system during low- gravity maneuvers, Ratvasky measured tail-flow conditions and elevator settings for cruise, hold, and approach, as these conditions would be simulated in impending IRT tests. They determined the range of tailplane inflow angles for the flap, speed, thrust, and normal accelerations to be tested with ice shapes. Ratvasky was able to conduct TIP tests in the IRT in February 1996. The Twin Otter airfoil was subjected to a variety of icing cloud conditions, while different air- speeds, angles of attack, and elevator deflections simulated the cruise, holding, and approach phases of flight. Following each test run, technicians made ice tracings and took photographs of the resultant ice shapes. At the end of the night, they made a mold of a 15-inch span of the final ice accretion. Skilled craftsmen in the model shop then extracted multiple polyurethane castings from the mold to have a full-span ice accretion for later aero-performance tests in the Ohio State tunnel in August 1996. Finally, everything was ready for flight tests with the various ice shapes that had been developed in the IRT and Ohio State tunnel. The climax of the test program came between July and September 1997. Researchers Ratvasky and Judith Foss Van Zante took data as pilots Ranaudo, Robert McKnight, and William Rieke searched for the bound- aries of tailplane stalls with various ice shapes. On 17 September, Ranaudo passed the New Challenges 145

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